CASE SCHOOL applied0 Science A v^ r r- y \ ^S^£ p te-^ _ *>(JjS \ ' y v ^— ^ ) ] DEPARTMENT PHYSICS \ Class SZ I . / S^elf V Date Accession ~7 3 ( ) 0 WASHINGTON OBSERVATIONS FOR 1885.— APPENDIX III THE SOLAR PARALLAX AND ns RELATED CONSTANTS, INCLUDING THE FIGURE AND DENSITY OF THE EARTH. BY WM. HARKNESS, PROFESSOR OF MATHEMATICS, U. S. NAVY. DEPARTMENT OF PHYSICS Case School of BpplteD science CLEVELAND OH I© WASHINGTON: GOVERNMENT PRINTING OFFICE. i 8 9 I . TABLE OF CONTENTS Tag*. 1. Introductory 1 2. Algebraic notation, and citation of authorities 1 3. Relations between units of length 3 4. Size and figure of the Earth 3 5. Length of the seconds pendulum 6 6. Length of the year 10 7. The eccentricity of the Earth's orbit, and the constant (1+x) 11 8. The length of the month 12 9. The constants//, m, (1-\-h'), e2, y and I, pertaining to the Moon 10 10. Observed value of the parallactic inequality of the Moon 18 11. Observed value of the lunar inequality of the Earth 19 12. Observed value of the lunar parallax 20 13. The constant of precession 22 14. The constant of nutation 25 15. The constant of aberration 25 16. The light equation 28 17. V, the velocity of light in vacuo 29 18. Masses of the planets 33 19. Trigonometrical determinations of the solar parallax 51 20. General forms of the conditional equations 56 21. The least square adjustment 64 22. Numerical values of the corrections by adjustment 6S 23. Additional formula? for precession 73 24. The density, flattening, and moments of inertia of the Earth 89 25. Uncertainty in the value of £, and its effect upon the other constants 102 26. Mass of the Moon from observations of the tides 112 27. A more comprehensive least square adjustment 121 28. The electric constant, v 135 29. Supplementary data 136 30. Summary of results 138 31. Concluding remarks 142 32. Bibliography 146 Index 165 m ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 1.— INTRODUCTORY. Hitherto it has been customary to endeavor to determine the solar parallax as if it were an independent constant, and the result is a mass of discordant values, all of which are more or less affected by constant errors, and none of which command any- thing like universal assent. But, in truth, the solar parallax is not an independent constant. On the contrary, it is entangled with the lunar parallax, the constants of precession and nutation, the parallactic inequality of the Moon, the lunar inequality of the Earth, the masses of the Earth and Moon, the ratio of the solar and lunar tides, the constant of aberration, the velocity of light, and the light equation ; and according to the most elementary mathematical principles, it should be determined simultane- ously with all these quantities, by means of a least square adjustment. No other method offers anything like so much promise of eliminating the ever present constant errors, and therefore an attempt will be made to develop it here. The equations connecting the quantities mentioned are known, but for the sake of completeness their derivation will be given. The theory of these equations and the discussion of the numerical quantities which they involve are entirely distinct subjects, and as clearness will be gained by separating them, we will begin by investigating the numeri- cal values, both of the constants, and of the quantities to be adjusted. 2.— ALGEBRAIC NOTATION, AND CITATION OF AUTHORITIES. Except where otherwise stated, the following notation will be employed in alge- braic formula? : a zz equatorial semi-axis of the globe of the Earth, if that body is regarded as a spheroid ; or major equatorial semi-axis, if it is regarded as an ellipsoid. a' •=. minor equatorial semi-axis of the Earth, when that body is regarded as an ellipsoid. b — polar semi-axis of the Earth. ax = that distance between the Earth and the Sun which would satisfy Kepler's third law. * In its original form this paper was a private investigation, and as such was read before the Philosophical Society of "\\ ash- ington on October 13, 1888. Since then it has been taken up in connection with my official work, to which it is closely related, and many important details have been added. — W. H. 6987 1 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. a2 zz that distance between the Earth and the Moon which would satisfy Kepler's third law. E zz the combined mass of the Earth and Moon. E' zz the mass of the Earth, excluding- the Moon. e zz eccentricity of the globe of the Earth. \ (i + x') M = regression of Moon's node, relatively to the line of equinoxes, in 365^ days. v zz the heliocentric longitude of the Earth. v' zz the geocentric longitude of the Moon. p zza factor, varying with the latitude, such that the radius of the globe of the Earth at latitude

' zz geocentric latitude. ip zz the luni-solar precession. ip! zz the general precession. co0 — the mean obliquity of the fixed ecliptic at the initial epoch. go — the obliquity of the fixed ecliptic at the time t. &>! zz the obliquity of the moving ecliptic at the time t. For a list of the principal works consulted in the preparation of the present paper, and an explanation of the method by which they are cited in the foot-notes, the reader is referred to the section on bibliography, pages 146-165. 3.— RELATIONS BETWEEN UNITS OF LENGTH. For interchanging the various units of length employed by different authors, the following ratios, based upon Gen. A. R. Clarke's determinations,* will be used throughout this paper : Logarithms. i meter — 3*280 869 33 feet 0*515988934 1 kilometer rzO"62i 376 767 mile 9793 355 OI1 1 toise zz 6-394 533 48 feet 0*805 808 865 1 toise zz 1*949036318 meters 0*289819931 1 Paris line zz 0*002 255 829072 meter 7*353 306 189 1 statute mile zz 1*609 329 561 kilometers 0*206 644 989 1 English inch = 0*025 399 772 meter 8*404 829 820 4.— SIZE AND FIGURE OF THE EARTH. When the Earth is regarded as a spheroid, let a be its equatorial and b its polar semi-axis; and when it is regarded as an ellipsoid, let a and a' be respectively its major and minor equatorial, and b its polar semi-axis. Then the flattening will be given by the formula a — b , x £=— — (0 a and the ratio of the axes will be a:b=l:--i (2) e e In 1 799 Mlchain and Delambre found from a combination of the arc of 90 40' which they had measured between Dunkerque and Barcelona with the arc of 30 07' measured in Peru by Bouguer and La CoNDAMiNEf Log. a (in meters) zz 6*804 53°5 °74 Log. b (in meters) zz 6*803 22&2 744 Whence a — 6 375 738*66 meters zz 20917 965 feet b zz 6 356 649*63 meters zz 20 855 ^37 feet frz 1/334 *'3. P- '57, and 23, p. 280. f2S. T- 3. PP- >96 and 432- 4 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. In 1830, from fourteen meridional arcs having- an amplitude of 590 29', and four arcs of parallel having an amplitude of 220 41', Sir (then Professor) George B. Airy found * a=. 20923 713 feet b — 20853 810 feet £— 1/299-3249 In 1 84 1, from ten meridional arcs having a total amplitude of 500 36', to which he applied a more rigorous analysis than ha,d before been used, Bessel found f a = 3 272 077' 14 toises = 20923 407 feet b =. 3 261 139*33 toises =r 20 853 465 feet €= 1/299-1529 In 1858, from a discussion of eight meridional arcs having a total amplitude of 670 08', General (then Captain) A. R. Clarke found, when the curvature of the meridians was not restricted to an elliptic form J a — 20927 197 ±385 feet & = 20 855 493 ±257 feet £= 1/291-8554 And when the curvature was restricted to an elliptic form§ a =z 20 926 348 rb 1 86 feet £ = 20855 233 ±239 feet £ = 1/294 2607 In 1859 General T. F. de Schubert advanced the idea that the well-known dis- cordances between the astronomical and geodetic differences of latitude and longitude of points upon the Earth's surface arise mainly from the assumption that the Earth is a spheroid, when in truth it is an ellipsoid ; and, in accordance with that hypothesis, he found from eight meridional arcs having a total amplitude of 72 ° 37' || a = 3 272 671-5 toises = 20927 207 feet a = 3 272 303-2 toises rz 20924852 feet 3 261 467-9 toises = 20 855 566 feet 6 = In i860 General A. R. Clarke repeated General de Schubert's investigation by applying a much more exact analysis to five meridional arcs having a total amplitude of 760 35'. He founds a=z 20 926485 feet a' = 20921 177 feet 6=20853 768 d= 953 feet •17, p. 220. t'9. pn6. t 2i, p. 765. §21, p. 771. || 26, p. 31. Tf 22, p. 39. ON THE SOLAR PARAL1 \\ AND ITS RELATED CONSTANTS. c In 1866 the comparisons made at Southampton showed that the hitherto accepted relations of the principal standards of length were slightly erroneous, and to correct the error thence arising- General Clarke recomputed the axes last given, and found* a zz 20926 350 feet a zz 20919 972 feet b zz 20853 429 feet By modifying his equations so as to make them represent a spheroid, he found from the same dataf a zz 20 926 062 feet &zz 20 855 121 feet e= 1/294-9784 In 1878 the serious uncertainty respecting the unit of length employed by Colonel Lambton in the measurement of the southern half of the Indian meridional arc had been remedied by a complete remeasurement of that part of the triangulation ; the latitudes of many stations in it had been determined ; the length of the arc had been increased from 21 ° 21' to 230 50'; and an arc of longitude extending through io° 28' had been measured. The data available for determining the size and figure of the Earth were then the Russian arc of 250 20', the Anglo-French arc of 220 io', the Indian meridional arc of 230 50', the Indian longitudinal arc of io° 28', the Cape arc of 40 37', and the Peruvian arc of 30 07'. From these six arcs, having a total ampli- tude of 890 32', General (then Colonel) Clarke found J azz 20 926 629 feet a! zz 20 925 105 feet 6zz 20 854 477 feet In 1880, after considering the ellipsoidal theory, and calling special attention to the fact that sufficient data are not yet available for fixing definitively the form of the Earth, General Clarke reverted to the theory of a spheroid, and found from the arcs he had employed in 1 878 § a z= 20 926 202 feet & zz: 20 854 895 feet (3) These last values will be adopted in the present paper. From them we have (4) a — b _ a 293-4663 a2-b2 e2 — - zz 0-006803 481 019 (5) a1 72 tan cp' — , tan cp — ( 1 — e2) tan cp — 0*993 I96 5 1 9 tan cp (6) a2 _ 1 — e2 (2 — e-) sin2 g>_ cos cp / x ,a P — — 1 — c- sin2 cp cos cp' cos {cp — cp') *23, p. 285. U3, P-287. {24, p. 92. ? 13, p. 319- 6 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. And with sin cp z= \/&

P-352. ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. J And from a combination of his own stations, those of the British survey, and those of the French arc; in all 25 stations, having latitudes ranging from -f- 79° 50' to — 12° 59', he found / =139-0 15 20 + 0202 45 sin2 cp inches zr 0-990977 +0*005 l42 sin2

*38.P-36- t '°» T. 2, p. 466. J 17, p. 230. ^15, T. i,p. 367; 34. PP- 32-33. and l6> T- 2'P-464- ||39»P-3I6- 8 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. In order to reduce this to the standard form, let us assume I — 439-2923 + x + (2-2940 + y) sin2

successively equal to o°, 200, 400, 6o°, and 8o°, and compar- ing- the resulting values of / with those given by Unferdinger's expression, we shall obtain the observation equations o zz x + o-oooo y — 32 ozza; + o-i 170 — 10 o zz x : + 0-4 1 3 2 +12 ozz.r + 07500 —22 o zz x + 0-9698 — 78 where the absolute terms are in units of the fourth decimal place. The resulting normal equations are o zz + 5-0000 x + 2-2500 y — 1 30-0000 ozz+ 2-2500 +1-6874 — 88*3560 Whence rrzz + 6-093 057 2/ = + 44'23?654 and by substitution in (9) Izz 439-292 9 + 2-29842 sin2

] meter zz 0-990 918 + (0*005 262 + 14) sin2 cp meter For convenience of reference the preceding results are collected in Table I. In the case of Unferdinger's formula, the value of I for latitude 45 ° was computed from his original logarithmic expression, and not from that in the third column of the table. Table I. — Formula' for the Length of the Seconds Pendulum. Date. Author. / in meters. /(or

■=. yi, formula (13) gives I — 3-256 872 English feet. (14) *i3(P. 348. t">>T-2.P-428. IO ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 6— LENGTH OF THE YEAR. If we put m for the quantity by which the Sun's mean sidereal motion in 365^ days exceeds 3600, then the length of the sidereal year will be given by the expression T = ^{i--^ + (-^)-ete|days (15) 3600 ' V36C According to Hansen and Olufsen,* m = — 22-56009"; whence, by formula (15) T — 365-256 358 192 days — 365* o6h 09™ 09-347 88 According to Le Verrier the mean sidereal motion of the Sun in 365^ days isf 1 295 977-382 34" + 00603". Whence, mzz— 22 557 36"; and by formula (15) T — 365-256357422 days=:365d o6h 09111 09-281 28 As the perturbations of the Earth are not taken account of in precisely the same way by Hansen and Olufsen and by Le Verrier, the resulting values of the Sun's mean sidereal motion given by these two authorities are not rigorously comparable, but the systematic difference is very small. Neglecting it, we take the mean of the two values of T just found, and thus obtain for the length of the sidereal year, expressed in mean solar time T = 365*2563578i days — 365* o6h 09m 093 14":= 31 558 1493 H seconds (16) And the number of mean solar seconds in a sidereal day is If we put 4 = 86 400* X llVAlllll = 86 1 64 099 65e 366 2^63578 m-\-rp1zza-\-bt (17) (18) where tpx is the secular part of the general precession, the expression for the length of the tropical year will be -(^-(W?)M+etc- T' = 365Ja (19) Taking for m the mean of the values given respectively by Hansen and Olufsen, and by Le Verrier, namely, m — — £ (22-560 09"+ 22-557 36") = — 22-558 72" Uo, p. 1. t4'» PP. 52 and 98. ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. II and putting m lf>l = + 50*236 2 2/'-r-0,02 2 044"( -— '- *-) V 100 J we have m+^1=4- 27-677 50" 4- 002 2 044 Y* ~ 1 85°) Whence, by formula (19), * T = 365-242 1 99 853d - 0000 006 2 1 2 4^~l85°A = 365d o5h 43m 46-067'- 0-536 75'(*~^5°) (20) The variation in the length of the sidereal or tropical year produced by a small change in the adopted value of m, formula (15), or a, formula (19), may be readily found from one or other of the expressions dT = — 24-3 576- }4i,p. 102. , 2 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. According to Le Verrier* . and as we have put it follows that r — «! ( i + 2 ") o1 = r (i + x) 3W Here « is the Earth's mean sidereal motion, and a is a quantity depending upon the perturbations of that motion by the other planets. For the numerical values of these constants Le Verrier found f Whence Log. n zz6i 12 60 i zz the secular part of the general precession. X zz sidereal movement of the solar perigee in 365^ days. n" zz the Moon's mean sidereal motion in 365^ days. m," zzthe Moon's mean synodical motion in 365^ days. n2" zzthe Moon's mean tropical motion in 3651 days. w3// zzthe Moon's mean nodical motion in 365^ days. n" zzthe Moon's mean anomalistic motion in 365^ days. *8, T. 2, pp. 30, 31, and 60. t8»T- 2> P- 59. and 41. P- "■ ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 13 The mean motion of the Moon used by Damolskai; can best be found by taking from his Table II* the mean longitudes for the years — 300 and — 2300 and dividing their difference by 2000. The resulting mean tropical motion in 365^ days is 5347-420869 125 centesimal degrees or, expressed in sexagesimal seconds, of which there are 3240 in each centesimal degree, 17325 643-616 o". To that motion Airy found the correction -j- 0-596";! and as he used Bessel's value of the precession, which for the epoch i8oo-o is 50-2235", his value of the mean sidereal motion of the Moon in 365^ davs is 17325643-6160"— 50-223 5"+ 0-596"= 17 325 593-988 5" and adding the secular acceleration J n"= 17 325 593-985 8''+o-2i64''(^^) (26) It is easily seen that and also n" = ^(g + co-&-^) (27) nf^z^g + cD-v'+x) (28) But when the numerical values of the quantities in the right hand members of these equations are substituted from Hansen's Tables de la Lune, pp. 15 and 16, a discord- ance appears in the terms involving the square of the time; equation (27) giving for the coefficient +0-00033260", while equation (28) gives +000040419". Taking the mean of these two numbers, Hansen's value of the mean sidereal motion of the Moon in 365^ days is // // , r "ft — i8oo\ n — 17325 593'973 * +0-24360 ^- J . t:o 11ft— i8oo\ + 000036840 ( J «-i8ooV (29) In his "Researches on the Motion of the Moon," Newcomb found that Hansen's tables required the correction § - ri4" -0-291 7" (*- i8oo)-3-86"(^~l8ooY *5o. p. 3- t44, P-io. t44, P- 8. § 6o, pp. 268 and 274. H ON THE SOLAR RARALLAX AND ITS RELATED CONSTANTS. to the mean longitude of the Moon; and the correction + o*io" (t — 1800) to the motion of the Moon's node. Or, in other words, if we put g0, g'0, go0, go'0 and &0 for Newcomb's corrected values of the quantities g, g', go, go', and ©, then ^=//-i-i4'/-o-29i7'/(^-i8oo)-3-86''(^I^)2 GOQ — GO — O'lO" (t— ISOO) (30) co'0 — go' — o* i o" (t — 1 800) 0O -O —OIO" (£— I800) and the substitution of these corrected values in equations (27) and (28) gives n" =*t(g + Co-0-zpl)-o-29i7" -0-0772 (^^) (3i) d , . / , n // st— 1 8oo\ f N = jt(g + oo-oo'-\- X) -0-2917 -0-0772 ( ioq j (32) Newcomb's value of the mean sidereal motion of the Moon in 365^ days is there- fore (33) n" = 17 325 593-68: 4" + 0166 40" (j-^) /:o // ft— l800\2 + OOOO3684O ( J If we put n" = a + bt + ct2 (34) the expression for Tlf the length of the sidereal month, will be T.=36tf£.3y = 473364oo°" \ ,-*<+(*;-«>-«*■ 1 05) a+o£ + cr a ( a Vflr ay > to terms of the third order in (£ — 1800). Formulae (26), (29), and {t>Z) are 0I> tne same form as (34), and the several values of T: are to be determined from them bv substituting in (35) the values of a and b which they contain. In view of the uncertainty as to the true value of the secular acceleration of the Moon's motion, the terms depending upon the square of the time can have no real significance, and will be neglected. From (26) and (35), according to Airy Tjzz 27-321 66o682d — coooooo 341 25d( — j = 2 7do7h 43m 1 1 -483s - 0-029 484s (l ~ 1 8o° ) V 100 J ON THE SOLAR PARALLAX AND IIS RELAT1 D < ONSTANTS. 15 From (29) and (35), according to Hansen T1=. 27321 660 702'' — 0-000000384 i5df -J ^ 1800 \ (37) -27do7h 43m n-4848-oo33 191*^ ^ J And from (33) and (35), according to Newcomb Tx = 27-321 661 i62d — o-oooooo 262 4od( — j z= 2 7d 0711 43m 1 1 -524s — o-02 2 67i8( — \ Equations (36), (2,7), and (38) yield the following values for the mean length of the sidereal month at the epoch 1850-0, expressed in mean solar seconds Airy 2 360 591-468" Hansen 2 360 591-467 (39) Newcomb 2 360 591-513 For the mean svnodical, tropical, nodical, and anomalistic motions of the Moon we have ni" = ^-g' + C0-00') -0-2917" -00772" 0=^) (4o) <=|(j+fi,-e)-o-29i7"-oo772"(^^2) (40 *3" = I (9 + •) -0-3917" -00772" (tj=) (4») „ « = I W - o-29 . 7" - 00772" (^5) (43) where in each case the literal part of the expression is Hansen's value, and. the numeri- cal terms are Newcomb's corrections. Of these expressions the most important is (40). Hansen's value for it is nl' = 16 029 616-5331" + 0-243 824" ( ^q00) ,, 1 t — i8oo\ m, (44) 11 si — i8oo\ n /l — iouu\ + 0-00040419 (- IOO-J and Newcomb's value is // rr /- II ft iSOON 11,"= l6 029 6l6-24I4 +OI66 624 ( ) (45) + 0-00040419 (^ ioq j i6 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. (46) (47) Substituting- these values of w/' in formula (35), and neglecting the terms involv- ing the square of the time, the mean length of the synodical month comes out, according to Hansen 29-530 587 898d — o-ooo 000 449 1 9d ( — -^ = 29d i2h 44m 02794a-o-038 8io8^~l8o°^) and according to Newcomb 29530 588 435d — o-ooo 000 306 96d f — \ — 29d i2h 44m 02-841" — 0*026 522s ( — j As a check on the preceding computations, we may employ the relation Tx (T + T2) = TT2 (48) where T, Tx and T2 are respectively the lengths of the sidereal year, the sidereal month, and the synodical month. With the values of these quantities from (16), (38) and (47), we find T^T + TOzz 10 786-235 1 74 5 days TT2 zz 10 786-235 1 "J2> 6 days For the other months, at the epoch 1850-0, we have from equations (41), (42), and (43), by substituting the values of g, go, and © from Hansen's lunar tables, and neglecting Newcomb's corrections %"= 17325644-33' *h"= 17 395 27364 iu" — 17 179 158-87 (49) whence Mean Tropical Month =27-321 581 292* zz 2fx ojh 43™ 04-624" Mean Nodical Month — 27-212 219 238d zz 27d 0511 05™ 35742s (50) Mean Anomalistic Month zz 27554 550463d zz 2 7d 1311 i8m 33- 1608 9.— THE CONSTANTS M, ™, (1 + «'), e2, y, AKD I, PEETAIXING TO THE MOON. For the regression of the Moon's node relatively to the line of equinoxes, in 365^ days, Hansen's lunar tables give * d .,, st— 1800 x ^ = ~^(0 + ^) = -69679'6l9I''+O"I4I36,'(^Too~) (5° Whence, for the epoch 1850-0 /^zzi9° 21' 19-5484" zz 0337 815 984 of radius (52) *54, PP- 15-16- ON THE SOLAR PARALLAX \NI> ITS RELATED CONSTAN I 7 Or, with Professor Newcomb's correction, from (30) ju=iq° 21' 194484" = 0337 815 499 of radius (53) The ratio of the mean sidereal motions of the Sun and Moon results immediately from (39) and (16), thus m=S= 2360 59i-5i3; = 0.07 8 II2 (54) By putting 0^ = ^(1 + x') and comparing this with the expression given by Delaunay for the constant part of the lunar parallax, namely* i=ij,+('+u«y-is*'-«rf| (5s) rx (U ( \o 4 ; 255 40 > we find ■+"'='+(>;'■■ )'"=-^"',-48'"s (56) Whence, by substituting the values of el and m from (24) and (54) 1 + *' = 1 'ooo 908 743 (57) From all the lunar observations made at Greenwich between the years 1750 and 1847, inclusive, Sir G. B. Airy found for the coefficient of the first term of the equa- tion of the Moon's center f 22 639-06" (58) Professor Newcomb found that for the same term Hansen used in his lunar tables % 2264015" (59) and from all the meridian observations of the Moon made at Greenwich between the years 1847 and 1874, and at Washington between the years 1862 and 1874, inclusive, Newcomb found the correction —0-57" to (59), § which thus becomes 22639-58" (60) Taking the mean of (58) and (60), giving the former double weight, and equat- ing the result to its analytical equivalent,|| we obtain 22 639-233' = 2 r, - 1 e2a + ^ ef- *52, T. 2, p. 914. Compare also 63, T. I, pp. 664 and 674. ?6i,p. 29, and 62, p. 69. 1 44, p. 13. 1 62, P- 69. II 52. T. 2, p. 804, equation (7). 6987 2 !^ ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. Whence e2— 1 1 323880" =0054 899 720 of radius (61) For the coefficient of the first term in the development of the Moon's latitude, expressed as a function of the Moon's true longitude, Airy found from the Greenwich observations made between the years 1 750 and 1847, inclusive,* 18 535-55"; but when expressed as a function of the time, this becomes, according to Delaunayj 18461-26" (62) Professor Newcomb found that the value of the same coefficient implicitly con- tained in Hansen's lunar tables is J 18 461 629" ; and to that Newcomb found a correc- tion of —015" from the Greenwich and Washington observations of the Moon made between the years 1862 and 1874. § His corrected value is therefore 18461-48" (63) Taking the mean of (62) and (63), giving the former double weight, and equat- ing the result to Delaunay's analytical expression for it,|| we have 1 8 46 1 -33" r= 0-089 503 054 of radius — 2/ — 2/tv — - ys + 7 ye2* + - y*e£ 5 - ye* 4 32 4 H4 whence, with the value of e2 from (61) y — 0044 886 793 (64) As y is the sine of half the inclination of the Moon's orbit to the plane of the ecliptic, (64) gives 1 = 5° 08' 43-3546" =0089803 757 of radius. (65) 10.— OBSERVED VALUE OF THE PARALLACTIC INEQUALITY OF THE MOON. From the nature of the case, the observations for determining the coefficient of this inequality must be made partly upon the first, and partly upon the second limb of the Moon, and thus they involve all the systematic errors which may arise from the different conditions under which these limbs are observed, and all the uncertainty which attaches to our knowledge of the Moon's semi-diameter. The following values are perhaps the best hitherto obtained : 1. From his discussion of the lunar observations made at Greenwich between the years 181 1 and 1851, Sir G. B. Airy concluded that the most probable value of this coefficient is 1 24-7" H 2. Professor Newcomb found that the value deduced by Hansen from the Green wich and Dorpat observations is 126-46" ** * 44, p. 21, and 45, p. 27. J 62, p. 76. ||52, T. 2, p. 862, equation (1 ). ** 232, p. 23. 1 52, T. 2, p, 802. g6i,p. 36. tf44,p. 16. ON" THE SOLAR PARALLAX AM) ITS RELATED <<>NST.\NIS 19 3. From 2075 lunar observations made at Greenwich between the years 1848 and 1866, Mr. E. J. Stone found 1 25 36" ^ 04" ; the probable error being estimated.* 4. From the lunar observations made at Washington between the years 1862 and 1866, Professor Newcomb found 125-46". f 5. From an extended discussion of the whole subject, Messrs. Campbell and Neison found, cither 1 25 64" ±009", or 12464" ±0*2 5", according as a certain hypo- thetical 45-year term was or was not admitted into the lunar theory.J 6. From a comparison of Hansen's lunar cables with some 1 600 observations of the Moon, made with the Greenwich transit circle between the years 1862 and 1877, Mr. Edmund Neison found 1 253 1 3" ±0-046" ; but he thought it probable that that value might require diminution by 073" on account of the before-mentioned hypo- thetical 45-year term.§ The controversy carried on in the Monthly Notices of the Royal Astronomical Society by Mr. Stone and Messrs. Campbell and Neison, during- the years i88o-'82, shows that the entire mass of existing lunar observations must be thoroughly redis- cussed before a definitive value of the parallactic coefficient can be obtained. Respect- ing- the data given above, it may be remarked that the values in paragraph 5 are superseded by that in paragraph 6, and that the mean of the values in paragraphs 1 and 2 is nearly the same as the values in paragraphs 3, 4, and 6. All questions of weights may therefore be disregarded, and by taking the arithmetical mean of all the values except those in paragraph 5, we find Q= 125-46" ±0-35" (66) where the probable error is estimated to be one-fifth of the difference between the greatest and least values. 11.— OBSERVED VALUE OF THE LUNAR INEQUALITY OF THE EARTH. The magnitude of the coefficient of this inequality is only about two-thirds that of the solar parallax, but as it depends upon differences of the sun's right ascension, which is always observed in precisely the same way, it should be free from constant errors, and can therefore be determined with great accuracy. The following are the best available data : From observations at Greenwich, Paris, and Koenigsberg. made during the periods stated, Le Vekeiek found || Greenwich 18 16-1 826 L =: 6-45" Greenwich 1 827-1 850 656 Paris 1 804-1 8 14 661 Paris 18 1 5-1 845 647 Koenigsberg 18 14-1830 643 Mean = 6-50 ± 0023' '65, p. 271. t232, p. 24. t46, p. 467- §59. P- 409- ||4i,l>ioo. 20 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. Professor Newcomb found the following additional values* Greenwich 1 85 1-1 864 L = 6 56" ± 004" Washington 1861-1865 6-51 ±007 Giving- these three results weights inversely proportional to the squares of their probable errors, namely. 9 26, 3 06, and 1, we obtain L- 65 14" ±0016" (67) lli. — OBSERVED VALUE OF THE LUX Alt PARALLAX. For the determination of this constant, all the data at present available are based upon declinations of the Moon, observed respectively in Europe and at the Cape of Good Hope. From a comparison of Lacaille's observations at the Cape with those made at Greenwich, Paris, Berlin, and Bologna, during the same period, namely, from June, 1 75 1, to February, 1753, Professor Olufsen found f x = sin P — 0016 512 t,^ +0024 492 01 £ — 0000 001 62 dh or, multiplying by 3423 3"/ sin 3423 3" = 206 274-28 P = 3406069" + 5052-072" e — 0334" dh ± 0.45" (68) where £ is the Earth's compression, and dh the error in the longitude of the Cape, expressed in minutes of time. Neglecting dlj, we have from (4) 293466 whence P = 3406 069" +17-21 5' = 3423284' ± o 45" (69) From his own observations of the Moon at the Cape, combined with observations made at Greenwich and Cambridge during the same period, namely, from May, 1832, to May, 1833, Professor Thomas Henderson deduced two values of the lunar parallax ; one by comparison with Burckhardt's tables, and the other by comparison with Damoiseau's tables. As Burckhardt's parallaxes are now known to be erroneous, we have only to consider the result from Damoiseau's tables, which was J where P rr 342246'' + 5062" 5c — 0-05" St — o'i2 6s — 014 S.s' (70) Longitude of Cape Observatory ~ 1 h i$m 55s 4- r5^8 Sc = £ — 300 1 232, pp. 25-26. 1 74. P- 226. j 73, p. 294. ON ["HE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 21 and Ss and Ss' are corrections for any constant differences which may have existed in the values of the Moon's semi-diameter given by the different instruments, and the different observers. Neglecting Ss and Ss'} we have St = -o-3sa * i i OC Z= — — = 0-000 0/4 2 2 293'466 3OO Whence, from (70) P = 3422-46" +0-376" +0-018" = 3422-854" (71) By combining 123 observations of the Moon made at the Cape during the years 1830 to 1837, with corresponding observations made at Greenwich, Edinburgh, and Cambridge, Mr. Breen found* P =23422-696" — 0*013 St (72) where St is the correction to the assumed longitnde of the Cape, and the compression of the Earth is taken to be 1/300. With our value of the compression, namely, 1 / 293-466, and St = — o-35s, (72) gives P = 3422-696" 4- 0-376" + 0-005" = 3423-077" (73) Bv combining 239 observations of the Moon made at the Cape during the years 1856 to 1 86 1 with corresponding observations made at Greenwich, Mr. E. J. Stone found f P — 3422-707" ± 0-049" Mr. Stone does not state what compression he employed, but as 1/300 was then used both at Greenwich and the Cape, the same correction should probably be applied as in (71) and (73). That gives P = 3422-707" 4- 0-376" = 3423-083" ± 0-049" (74) Collecting our results, we have from (69), (71), (73) and (74), P=: 3423-284' according to Olufsen. 3422-854 according to Henderson. 3423-077 according to Breen 3423*083 according to Stone. When it is remembered that the first of these values is based upon observations made with old-fashioned quadrants, the second and third upon observations made with mural circles, and the fourth upon observations made with large transit circles, their agreement is remarkable. However, as the observations upon which the second result rests have all been embodied in the third, we will adopt the mean of the last two. and put P = 3423-08" ±0050" (75) If we assume the probable errors of the latitudes of Greenwich and the Cape to be ±0-05". then the probable error of P should be increased to ±o-i 21" *72,p. 137. t75. p- 16. 22 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 13.— THE CONSTANT OF PRECESSION. Putting ip and ipx respectively for the secular parts of the luni-solar, and of the general precession; go for the mean inclination of the equator of 1850 -f- 1 to the fixed ecliptic of 1850; and col for the mean inclination of the equator of 1850 + / to the ecliptic of 1850 + ^; then, according to Le Verrier and Serret, we shall have* ( 50371 Ao"+x + ooiAS"y + 0-1743" "' h_o-oooio8 8o6"^ ( + 00169" v"1 —0-057 5" v1T — o-oi2 4 ' vv ) go — &>„ + 0-000007 180" t2 (76) ip! = (50-235 72" + x) t + o-ooo 1 1 2 900 t2 ( 0-475 66" +0-005 3" k + 0-288 8"^ I * a>. — &>0— < ^/J „ ' ... ^ ' . „ }t — o-ooo 001 490 t~ X +0-008 3" ^" + 01601"^+ 0-013 1" vx s where a; is a small unknown correction to the precession constant, and t is counted in Julian years from the epoch 1850-0. From the adopted masses of the planets, given on pages 42 and 48, we have v =-0655353 y' rr — 0^007 004 vm = — 0-133558 vlT:= + o-oo2 339 vv — + o-oo2 970 Whence, by substitution in (76) ip = (50-358 25" + ./) t — o-ooo 108 806" e go =: oo0 + OOOO 007 1 80" t2 Xp-L = (50-235 72" + X) t + OOOO I I 2 9OO" t2 a>! = go0 — 0-46947" f-o'oooooi 490" t2 (77) From the series of observed values of the obliquity of the ecliptic given by Le Verrier,! and with the theoretical value just found for the annual change of the obliquity, we deduce for 1850-0 G>0=23° 27' 31-36" ±0-345" (78) To find the planetary precession, A, we have ^ — ^1 = A COS £ (GO + GJj) (79) where it will be sufficiently accurate to take cos %(go + g>i) — cos (a>0 — 0234 735" t) = cos &>„ + 0-234 735" tare 1" sin co0 (80) The substitution in (79) of the values of if>, rf>u go and cou from (77), (78) and (80), gives Whence 0-122 53 / — oooo 221 706" t2— A (0917 347 2+0-000000453 t) A— 0133570" t — 0000241 748" t2 (81) *8, T. 2, 1 . 174, and 83, p. 324. t4i. p. 51. ON THE SOLAR PARALLAX AND IIS RELATED CONSTANTS. Equations (77), (78) and (81) give ' ^ =50-358 25" +.r — 0-000217612" t ' ?? = 5°'235 72" +.r + o-ooo 225 800" t ' (U — o-I33 57" -0-000483 496" t sin co = 0398 088 1 2 -f 0000 000 000 03 1 9 t2 cos co = 0-9 f 7 347 1 7 — o*ooo 000 000 01 3 9 £2 And by substituting these values in the well-known expressions dd> dA (lib . m = — cos «>— - n=z ,- sin © dt dt dt 23 (82; we obtain m — 46-062 43" -f o-ooo 283 870" t -f 091 7 347 # w z= 20-047 °2" — o'ooo 086 629" t + 0-398 088 a? (83) For the epoch 17775, from a comparison of his own reduction of Bradley's observations with Piazzi's catalogue for 1800, Bessel found* m zz 46-034 002" n = 20*064 472 When Newcomb's correction for systematic errors in the right ascensions of the catalogues is applied,! namely, — o*43"/45 zz — O'ooo 555", these numbers become «r 46*024447" fizz 20-064 472 and their substitution in (83), together with t — — 72*5 years, gives from m, xzz — o*oi 8 97" from n, xzz-\- 0*028 06 Giving the result from m double weight, and taking the mean #r= — 0003 29" (84) For the epoch 1 790, from a comparison of Bessel's reduction of Bradley's obser- vations with the Dorpat observations, Otto Struve found the general precession to be 50*234 92" i 0*007 57". % Applying Newcomb's correction for systematic errors, § namely, —0*3 7" / 70 zz — 0*005 29"> tne precession becomes 50*22963". Formula (82) gives for the same epoch 50*222 17", and therefore £ = + 0*00746" (85) For the epoch 18447, fr°m a comparison of AVeisse's reduction of Bessel's zones with Schjellerup's catalogue, Nyren found || w = 46*026 5". Applying Newcomb's ♦76, p. 404. t^i.p. 108. +"85, p. 104. §81, p. 108. ||82, p. 571. 24 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. correction for systematic errors, namely,* + ro4"/36 -= +0*028 9", this; becomes m = 46*055 4", which being substituted in (83), together with £ = — 5-3 years, gives r — — o 006 03' (86) For the epoch 1829-7, from a comparison of Lalande's zones' with Schjellerup's catalogue, Dreyer foundf m — 46-066 6", which being substituted in (83), together with t = — 20-3 years, gives x = + 0-01082" (87) For the epoch 18050 Mr. Ludwig Struve made a comparison between Dr. Auwer's reduction of Bradley's observations and the Pulkowa catalogue of 1855, from which he found J m rr 46*041 7" + o-ooo 274 1" t where t is reckoned from the year 1800. His observed result for 1805-0 must there- fore have been m z=z 46 043 07" and the substitution of that in (83), together with £ = — 45*0 years, gives x = — 0*007 1 8" (88) Mr. L. Struve speaks highly of Dr. Bolte's Untersuchungen fiber die Priicessions- constante,§ but the present writer has never seen that work. Collecting our results, we have from numbers (84), (85), (86), (87), and (88) Authority. Value of x. General Precession. 1800. 1850. Bessel O. Struve Nyren Dreyer L. Struve Means // — 0-003 29 +0-007 4° — 0-006 03 +0010 82 — 0-007 J8 // 50-221 14 50231 89 502 1 8 40 50-235 25 50-217 25 50-232 43 50243 18 50- 229 69 50- 246 54 50-228 54 -fo-ooo 36 50-224 79 50-236 08 And by substituting the mean value of x in (yy) ip =(50-358 61" ±0-00248") ^- o-ooo 108806" t2 ^ — (50-236 08" ± 0-002 48") t + O-OOO I I 2 900" t2 (89) *8i, p. 109. 177. !>• 154- + 86, ]>. 30. jJ An inaugural dissertation, Bonn, 1883. ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 25 14.— THE CONSTANT OF NUTATION. The following- is an abstract of the most important determinations of the constant of nutation hitherto made : // // 1821. BRINKLEY, from 1618 zenith distances of 10 stars, measured at the observatory of Trinity College, Dublin, between the years 1S08 and 1820. (90, p. 347.) 9-25 ^0-05 1836. Busch, from 1949 zenith distances of 23 stars, observed at Kew and Wansted by BRADLEY during the years 1727 to 1747. (91, p. ^S.) 9-232^0031 1838. Robinson, from 6023 zenith distances of 15 stars, measured at Greenwich with the mural circle during the years 1812 to 1835. (113, p. 18.) 9-239 -J- 0052 1841. Lundahl, from more than 1200 zenith distances of Polaris, observed at Dorpat during the years 1822 to 1838. (99K'P- 33) 9-236 J- 0-040 1 84 1. C. A. F. Pf.ters, from 603 right ascensions of Polaris, observed at Dorpat by Struve and Preuss during the years 1S22 to 1838. (109, p. 161.) 9-216 -J-0020 1855. Main, from 173 zenith distances of y Draconis, observed at Greenwich with the 25-foot zenith tube during the years 183710 1847. (102, p. 1S6.) 9'323i°'°S9 1868. E. J. Stone, from 3250 zenith distances of Polaris, 51 Cephei, and 6 Ursx- Minoris, together with 1936 right ascensions of Polaris, all observed at Greenwich, with the transit circle, during the years 1 85 1 to 1867. (114, p. 249.) 9-134 -i- 001 1 187 1. Nyren, from 375 observations of ti Ursae Majoris, 1 Draconis, and oa Draconis, made at Pulkowa with the prime vertical transit instrument, during the years 1840 to 1862. (104, p. 30.) 9-244 -J- 0-0I2 1882. Downing, from 1041 zenith distances of y Draconis, observed at Greenwich with the reflex zenith tube, during the years 1857 to 1875. (92, p. 344-) 9'335 ±0-032 1885. De Ball, from 1867 right ascensions of Polaris, 51 Cephei, and A Ursae Minoris, observed at Pulkowa by Wagner during the years 1861 to 1872. (89, p. 42.) 9-217-^-0012 The probable errors attached to Brinkley's and Robinson's results have been taken from Peters's paper,* and that attached to Stone's result has been computed by the present writer. Giving- the determinations by Main and Downing half weight, because they rest upon a sing-le star, we have from the weighted mean of the whole series $ = 9-2331" ±0-0112" (90) Busch's determination should probably have been rejected on account of the errors discovered in his computations by Dr. AuwERS,f but its retention does not sen- sibly affect (90). The probable error of (90) is largely increased by the constant errors which evidently exist in the results found by Main, Stone, and Downing ; but as their determinations rest upon more than 6400 observations, made with three differ- ent instruments, it does not seem prudent to ignore them. 15.— THE CONSTANT OF ABEERATION. The following is an abstract of the best values hitherto obtained for the constant of aberration : // /' 1817. Bessel, from his discussion of Bradley's observations, (i, p. 123.) 20-475 1819. Piazzi, by the observations made at Palermo (5, p. 207) 20-229 1821. Br inkley, from 2633 zenith distances of 14 stars observed at Trinity College, Dublin. (90, p. 350.) . 20-372 1S22. F. G. W. Strive, from 693 differences of right ascension between 6 pairs of stars observed at Dorpat. (115, p. lxiv.) 20349 This result was subsequently corrected by C. A. F. Peters to 20-361" -J- 0-OIS6". See ill, p. 55. •109, p. 132. |88, p. 611. 26 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. // // 1828. RICHARDSON, from 41 19 zenith distances of 14 stars, observed at Greenwich. (112, p. 68.) 20-503 1836. BUSCH, from 1949 zenith distances of 23 stars, observed by Bradley at Kew and Wansted. (91, p. 338.) 20-212 -J- 0-038 1839. Henderson, from 231 zenith distances of Sirius, observed at the Cape of Good Hope. (95, p. 248.) . 2041 184 1. F. G. W. STRUVK, from 19 observations of v Ursa- Majoris in the prime vertical, at Pulkowa. (1 16, p. 290.) 20-493 ±0-040 1841. Lindenau, from 800 right ascensions of Polaris, observed at Greenwich, Konigsberg, Dorpat, Palermo, Milan, and Seeberg, during the years 1750 to 1816. (98, p. 62, and 1 1 1, p. 65.) 20-449 -J- 0-032 1841. C. A. F. PETERS, from 603 right ascensions of Polaris, observed at Dorpat. (109, pp. 142 and 180.) . . 20-425 -J- 0-017 1841. LiNDAiii, from more than 1200 declinations of Polaris, observed at Dorpat. (99}4>P-37-) 20-551-1-0.043 1842. Henderson, from 272 double altitudes of a1 and os Centauri, observed at the Cape of Good Hope. (96, P-370-) 20-523 -J- 0-065 1843. F. G. W. Struve, from 298 observations made upon 7 stars with the prime vertical transit instrument at Pulkowa. (118, p. 275.) 20445 ±0-011 1849. C. A. F. Peters, from Bradley's sector observations at Greenwich, (in, p. 23.) 20-522 -[-0-079 1849. C. A. F. Peters, from 704 declinations of 8 stars observed with the Ertel vertical circle at Pulkowa. (in, p. 138.) 20-481^0013 1849. Lindhagen, from 396 right ascensions of Polaris, observed at Pulkowa. (99, p. 354.) 20498 -|- 0-012 185 1. MACLEAR.from 391 double altitudes of n1 and a* Centauri, observed at the Cape of Good Hope. (100, P- 98) 20531 ±0-038 1852. Maclear, from 137 double altitudes of (i Centauri, observed at the Cape of Good Hope. (101, p. 152.) 20-594 -(- 0-049 i860. Main, from 486 zenith distances of y Draconis, observed at Greenwich with the reflex zenith tube, during the years 1852-1859. (103, p. 190.) 20-335 -[- 0-023 1882. Downing, from 1041 zenith distances of y Draconis, observed at Greenwich with the reflex zenith tube, during the years 1857-1875. (92^.344.) 20-378^0-040 1883. Nyren, from the series of observations made at Pulkowa, with the vertical circle, by Peters, Gylden, and Nyren ; with the transit instrument, by Schweizer and Wagner ; and with the prime vertical transit instrument, by F. G. W. Struve and Nyren. (106, p. 47.) 20-492 _[- 0-006 1888. A. Hall, from 436 observations of a Lyroe, made with the prime vertical transit instrument at Washing- ton, during the years 1862-1867. (94, p. 12.) 20-454 -J- 0-014 1888. KOstner, from 244 differences of meridian zenith distance of 7 pairs of stars, measured with the uni- versal transit at Berlin. (97, p. 45.) 20-313 -j-o-oi 1 A clearer exhibition of the facts will be attained b}r arranging the foregoing data somewhat differently, and in so doing Peters's reductions of Bradley's observations at Greenwich and Struve's observations at Dorpat will be accepted to the exclusion of those by Bessel and Struve himself; the determinations by Piazzi and Brink- ley will be omitted, the latter on account of the unexplained systematic errors exhib- ited by his declinations ; Busch's reduction of Bradley's observations at Kew and Wansted will be omitted on account of the errors discovered in Busch's computations by Auwers;* Struve's preliminary result from his observations of v Ursse Majoris in the prime vertical will also be omitted because the same observations are embodied in his final result, published in 1843; and Nyren's result will be separated into its original constituents. When these changes are effected, and the results are classed under the observatories furnishing the observations, we have the following exhibit: GREENWICH. // Peters, from Bradley's sector observations 20- 5 22 RICHARDSON, from mural circle observations 20503 Main and Downing, from zenith distances of y Draconis ■ . . . . 20-356 CAPE OF GOOD HOPE. Henderson, from Sirius 20-41 Henderson and Maclear, from a Centauri 20-527 Maclear, from (3 Centauri 20594 *88, p. 611. ON THE sol.AR PARALLAX AND [TS RELATED CONSTANTS. 27 DORPAT. // F. G. W. STRTJVE, from transit observations 20-361 LuNDAHL, from declinations of Polaris 20550 C. A. F. Peters, from right ascensions of Polaris 20425 PULKOWA. F. G. W. Strtye, from prime vertical" observations 20-445 C. A. F. Peters, from vertical circle observations 20481 LlNDHAGEN, from transit observations 20498 Nyren, from Gylden's observations with the vertical circle ... 20-469 Nyren, from his own observations with the vertical circle .... 20-495 Nyren, from Warner's observations with the transit 20-483 Nyren, from his own observations with the prime vertical transit 20517 BERLIN. Kustn'ER, from the zenith-telescope method 20-313 WASHINGTON. A. Hall, from observations of a Lyne with the prime vertical transit 20-454 VARIOUS OBSERVATORIES. Lindenau, from right ascensions of Polaris 2C449 Unmistakable evidences of constant errors are exhibited in these values of the constant of aberration — most notably in those found by Main, Downing, Maclear from ft Centauri, F. G. W. Struve at Dorpat, and Klstner. Nevertheless, it is diffi- cult to assign thoroughly satisfactory reasons for rejecting any of them. The Pul- kowa values are probably the most correct, but even they exhibit a range of 0-072". Perhaps no two astronomers would assign the same relative weights to the different determinations, and yet, within rather wide limits, it is precisely these weights which determine the magnitude of the final result If we take the means by observatories, we find Greenwich 20-460) Berlin 20313 Cape of Good Hope .... 20-510 Washington 20-454 Dorpat 20-445 Miscellaneous 20449 Pulkowa 20-484 and the arithmetical mean of the results from all the observatories, except Berlin, is a zz 20-467" ± 0-007" Again, if we take the arithmetical mean of all the results in the last general exhibit, tin; Pulkowa values will have relatively a little more weight than the others, and we shall obtain a — 20-466" ±o-oii" (91) which will be adopted. This lies almost exactly midway between Struve's classic value and that recently found by Nyrlx in his admirable paper on the aberration of the fixed stars. 2g ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 16.— TEE LIGHT EQUATION. The time occupied by light in traversing the mean radius of the Earth's orbit is usually called the light equation, and there are but two determinations of it from the eclipses of Jupiter's satellites, namely, Delambre's, published in 1792, and Glase- napp's, published in 1874. Delambre's value is 4932s. which he originally derived from 500 eclipses of Jupiter's first satellite, and subsequently revised without obtaining any sensible cor rection, although he used more than a thousand eclipses of the same satellite. The details of these investigations have never been published, and our knowledge of them is confined to the brief allusions contained in Lalande's Astronomy,* Delambre's Astronomy,f and Delambre's Tables e'cliptiques des satellites de Jupiter.} The last is the most explicit. Glasenapp's value is 50084s i ro28,§ which he derived from 391 eclipses of the first satellite of Jupiter, observed during the years 1 848 to 1 8 jt,. His memoir, although very valuable, is rendered almost inaccessible by being printed in the Russian lan- guage; but Mr. Downing has done something to remove that obstacle by publishing an excellent account of the work in The Observatory, vol. 12, pp. 173 and 210. In combining these two results the following facts must not be overlooked : 1. The eclipses used by Delambre were inferior to those used by Glasenapp on account of having been observed with less powerful telescopes, and possibly with less accurate knowledge of local time; but their inferiority can not have been great, because Delambre says of the eclipses he used, "il n'est pas rare de voir deux observations d'une mime eclipse diffe'rer entre elles dime demi minute, "|| and residuals of that magnitude are not rare among Glasenapp's equations. 2. After a thorough trial of Bailly's photometric method of correcting observa- tions of the eclipses of Jupiter's satellites, both Maskelyxe and Delambre abandoned it as useless;!! and yet Glasenapp's investigation is founded upon that very method, with some modifications whose value it is difficult to estimate. However, it will not escape notice that with the application of all his corrections Glasenapp found the light equation to be 500,84srb L028, while without them he found it to be 497 15s =b 1 208. The diminution effected in the probable error by the appli cation of the corrections is so small as to indicate either the failure of Bailly's method or the existence of periodic errors in the tables of the motions of the satellites. Glasenapp thought the latter hypothesis the more probable. 3. Delambre's result depends upon more than a thousand eclipses, while Glase- napp's depends upon onlv 391. And here we encounter the singular circumstance that the result which Delambre obtained from 500 eclipses was not sensibly modified when he used more than a thousand; while Glasenapp's result, which rests upon nearly 400 eclipses, differs largely from Delambre's. The existence of constant errors in one or both series of observations seems the most probable explanation. In view of these facts, it is not clear that Glasenapp's result is entitled to more confidence than Delambre's; nevertheless, we adopt the arithmetical mean of the two, *6,T. l,Tal)lesastronomiques,p. 238. J 127,]). vij. J,T. 3,p. 502. t.i.T-.i-PP- lo5- 1 06 and 502-507. $129, p. 131, and I28,p.2ll. ^ 3, T. 3, p. 507; 4, p. 746, and 12, v ol. 1, p. 266, sec. 464. ON I HE SOLAR PARALLAX ^ND ITS RELATED CONST A] 2<> thus giving Glasenapp rather more than double weight, and in view of tin; uncertainty of the result we attribute the whole of Glasia ait's probable error to it. In thai way we find Light equation, 9 = 497*0" rb L028 (92) which is almost identical with the result obtained by Glasenapp when he omitted his corrections to the observed times of the eclipses. 17.— V, THE VELOCITY OF LIGHT IN VACUO. The velocity of light can be measured between points upon the Earth's surface, either by the toothed-wheel method or by the revolving-mirror method. Both methods have been used, and the following are the principal results: Fizeau found V = 70 948 lieus of 25 to a degree m 3 1 5 324 kilometers =. 1 95 935 miles His experiments were made in 1849 by the toothed- wheel method, working across an interval of 8 633 kilometers = 5*364 miles, between Suresnes and Montmartre, Paris.* Foucault's experiments gavef V z= 298 574 =1= 204 kilometers— 185 527 i 127 miles He used the revolving-mirror method, and worked across an interval of only 20 meters = 65*6 feet, at Paris. His experiments were in progress from May to Septem- ber, 1862; but he based his final result upon the 80 observations made on September 18, 19, and 21. Cornu found, from the experiments which he made in August, 1872, V = 298 500 zb 995 kilometers = 185 481 d= 618 miles This result rests upon 658 experiments, made by the toothed-wheel method, work- ing across an interval of 10310 kilometers = 64064 miles, between l'Ecole Polytech- nique and Mont-Valerien, Paris. J Cornu found, from the experiments which he made in September, 1874, V — 300 400 rh 300 kilometers = 1 86 662 i 1 86 miles This result rests upon 546 experiments, made by the toothed-wheel method, work- ing across an interval of 22910 kilometers = 142357 miles, between the observatory and Montlhery, Paris. § Michelson found, from his experiments of June and July, 1879, V zz 299 910=1= 51 kilometers = 186 357 ±317 miles This result rests upon 100 experiments, made by the revolving-mirror method, working across an interval of 1986*23 feet = 0*3762 of a mile = 0*6054 of a kilometer, at the U. S. Naval Academy, Annapolis, Md.|| *I32,P.92. ti3S.P-224. } 130, p. 178. gi3i,p.A.298. ||I37. P- I57,andi39, p- 244. 30 "M I UK SOLAR PARALLAX AND ITS RELATED CONSTANTS. Young and Forbes found V = 301 3 84 ± 263 kilometers zz 187 273 ± 164 miles This result rests upon only 12 experiments, made in December, 1880, and Jan- uary, 1 88 1, by a peculiar application of the toothed-wheel method. The light from the collimator containing the toothed wheel was sent simultaneously to two reflecting collimators situated at different distances, but nearly in- the same straight line; and the observation consisted in determining when the images returned by these two collima- tors were of equal brightness. The toothed-wheel collimator was situated at Kelly House, Wemyss Bay, Scotland, and the reflecting collimators were located on the hills behind Innellan, across the mouth of the river Clyde, their distances being respectively 3-1884 and 3 4493 miles, or 5-13 13 and 5*5510 kilometers.* Newcomb found three results from the experiments which he made at Washington by the revolving-mirror method during the years 1880 to 1882. They are as follows:! («) From 148 experiments, made between June, 1880, and April, 1881, across an interval of 5*1019 kilometers — y 1702 miles, between Fort Myer and the U. S. Naval Observatory, V zz 299 709 kilometers zz 1 86 232 miles (b) From 39 experiments, made in August and September, 1881, across an interval of 7*4424 kilometers — 4-6245 miles, between Fort Myer and the Washington Monu- ment, V zz 299 776 kilometers zz 186 274 miles (c) From 65 experiments, made in July, August, and September, 1882, across the above-mentioned interval between Fort Myer and the Washington Monument, V zz 299 860 kilometers zz 186 326 miles If these results are to be combined, according to Newcomb we should assign the weight 2 to (a), 3 to (b), and 6 to (c) ; but he preferred to use (c) alone, on the ground that it is probably least affected by constant errors. Miciielson found, from his experiments in October and November, 1882, V zz 299 853 ± 60 kilometers zz 186322^=37 miles This result rests upon 23 experiments, made by the revolving-mirror method, working across an interval of 204935 feet zz 03881 of a mile zz 0*6246 of a kilometer, at the Case Institute, Cleveland, Ohio. J Now let us examine Cornu's results a little more closely. His experiments cover a wide range in the speed of the toothed wheel, and his mean result for each speed is given in Table II, where V is the velocity of light derived from an experiment in which i(2w— 1) teeth of the wheel passed during the interval between the departure and the return of the light, and p is the weight of V. With respect to the experiments •141, p. 269. f 140, pp. 194, 201 , and 202. % 139, p. 244. ON THIs SOLAR I'AKAI.l.AX AND ITS RELATED CONSTAN1 3' made in 1H74, it is to bo observed that the values of V are tin; weighted means of Cornu's uncorrected values of i(V + v) and \( U -f- a), the weights being taken just as Cornu gave them. Table II. — Cornu's experiments on the velocity of light. (130, p. 171 and 131, pp. A. 2(;ii-7.) Experiments of 1872. Experiments of 1874. 2» — 1 V P 211 1 V r 3 5 7 9 11 13 302-5 297-7 298-2 2988 297-5 300-5 129 2095 4 39' 4 783 924 260 7 9 11 '3 15 17 19 21 23 25 27 29 3' 33 35 37 4' 300 166 300 620 300 050 302 068 J99 960 300 100 300 224 jOO 359 300 500 300490 300304 300304 299 874 299 843 300083 299 55o 300 097 2 511 2 662 2 197 3 150 32946 28880 32 193 1 587 6 250 ij 122 54665 6727 25 047 29 400 6845 45 387 Helmert has pointed out that in the observations of 1874 V seems to diminish as {in — 1) increases; whence he infers that* V - V + y '.a — 1 (93) where V is the true velocity of light, and y is a constant depending upon the conditions under which the experiments were made. If we put Y-C + x V' = C + m (94) and substitute these values in (93), the observation equations for determining V take the form U 211— 1 (95) and the weighted normal equations will be of the form 0= ' [p]oc+ [2^TI]2/-I>m] 0 = [ 2^7] x + [(-2M - 1?] y ~ [s£J (96) *i36, p. 126. 32 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. Applying this to the observations made in 1872, with 0 = 2984, the weighted normal equations are 0 = + 12 582-00^+ 1 724730?/+ 188-200 0 = + i724'73^+ 255-969//+ 63-482 and their general solution is x = —0001 040912 P + 0-007013 710 Q y=z + 0007013 710 P — 0051 165396Q where P = + 188-200 Q = + 63-482 Whence x = + 0-249 344 700 ± 0844 7 y — — 1-928 ioi447±5'922 3 (97) V zz 298 649-3 i 8447 kilometers with which the residuals in the normal equations are + o-ooo 606 + o-ooo 085 the residuals in the weighted observation equations are — 5i'73 +11 53 +29-62 + 25-82 —2526 —32-19 and the probable error of an observation of weight unity is ±26 183 kilometers. Similarly, for the observations made in 1874, with 0 = 300000, the weighted normal equations are 0 = + 294 402 x+ 1 1 808 y— 51 012 357 0 = + 11 8082; + 546/y— 2455681 and their general solution is ioox = — 0002 561 621 1 P + 0*055 398 574 2 Q 1002/ = + 0-055 398 574 2 —1-3812204464 where Whence P = -5ioi2357 Q- — 2455681 x = — 53'668 960 ± 1 1 1 '8 kilometers y = + 5 658-249 626 ± 2 595 kilometers (98) V z= 299 9463 ±111-8 kilometers with which the residuals in the normal equations are + 5-4 and +o-2; the residuals in the weighted observation equations are + 1 7 009 — 2 251 + 21 194 — 79091 + 20395 + 32517 + 3420 — 25694 — 12 247 — 25 102 — 16975 — 38 006 + 20897 + 43 500 + 4287 + 45 423 — 2698 and the probable error of an observation of weight unity is ± 22 080 kilometers. ON THE SOLAR I XRAI.I.AX AN!) ITS RELAT] D CON I U 33 The values of V in (97) and (98) require to be multiplied b\ 1-000273 in order to reduce them to what they would have been in a, vacuum; and thus we find 1872. Vzz 298 731 ±845 kilometers = 185624^525 miles 1874. V = 300 028 ± J 12 kilometers = 186 430 i 69-5 miles which we shall employ instead of the numbers given by Count himself. Collecting- our results, we now have the following measurements <»f the velocity of light in vacuo per second of mean solar time, together with their estimated weights: Kilometers. Miles. Weight. 1849. FlZEAU .515 ;-4 195 935 O 1862. FOUCAULT 298574 185 527 I 1872. CORNU 29S 731 [85624 I 1874. COKNU 300028 186430 2 1879. MlCHELSON 2999IO 186357 3 1881. Voim; and Forbes 301 384 187 273 1 1882. Newcomb 299 860 186 326 6 1882. MlCHELSON 299 853 186 322 3 Fizeau's measurement is rejected on the ground that he himself regarded it as only a preliminary attempt. The weighted mean of all the other measurements gives V — 299 835 ± 1 54 kilometers rz 186 3 10 ± 95"6 miles (99) But if we consider only the four measurements whose weight is greater than unity, their weighted mean will give Vrr 299 893 i 23-0 kilometers ■=. 186 347 i 14*3 miles Ooo) Thus it appears that in either case we arrive at substantially the same value of V, but with widely different probable errors. We shall adopt the value (100), with a probable error equal to the difference between (99) and (100), namely, V — 299 893 i 58 kilometers ='186 347 i 36 miles (101) 18.— MASSES OF THE PLANETS. We need the mass of the Earth as one of the elements for finding the solar paral- lax, and the masses of all the other planets are required in computing the luni-solar precession from the general precession. The following are some of the most note- worthy determinations of these masses ; others may be found in Houzeau's Vade- Mecum de l'Astronomie. Reciprocals of the moss of Mercury. 1782. La Grange, from his hypothetical relation between the densities of the planet-, and their distances from the Sun. (167,]). 190.) 2025810 1841. Enckk, from the perturbations of the comet which bears his name, during its apparitions in 1819, 1825, 1828, 1835, and 1838, before perhelion. (153, p. 5.) 4 S65 751 185 1. Enckk, from the perturbations of the comet which bears his name, ( tables of the Sun. (41, p. 102.) 400246 1861. Le Verrier, in his tables of Mars. (8, T. 6, p. 309.) 412 150 1S72. Hn.i., from the motion of the node of Venus. (162, p. 36.) 427 240 1S76. Powai.ky, from observations of the Sun, made at Dorp.it. (181, p. 265.) 396980 1881. Tisseraxd, from the variation of the obliquity of the ecliptic. (189^.658.) 425500 1882. Newcomb, by estimation, from a consideration of various results. (177^.472.) 405000 Reciprocals of the mass of the Earth. [Values of the Earth's mass obtained from the solar parallax do not come into consideration here.] 1832. Plana, from the parallactic inequality of the Moon. (63, T. 3, p. 20.) (©without j.) 352359 1S63. 1 1 axsex, from the parallactic inequality of the Moon. {222, p. 11.) (©without (J.) 319 455 1872. Le Verrier, from the action of the Earth on the other planets. (172^.169.) (© — ([ •) . . • • 324490 1881. Tisseraxd, from a rediscussion of Le Verrier's equations. (189, p. 658.) (©^ ([ •) 325700 Reciprocals of the mass of Mars. 1782. La Grange, from his hypothetical relation between the densities of the planets and their distances from the Sun. (167, p. 190.) I 846082 1802. Delambre, from the perturbations of the Earth. (7,T. 3, liv. 6, chap. 16.) 2546320 1813. Kurckhardt, from the perturbations of the Earth. (151, p. 343.) 2680337 1827. Airy, from observations of the Sun made at Greenwich. (142^.30.) 3734602 1853. Hansen and Olufsen, in their tables of the Sun. (40, p. 1.) 3200900 1858. Le Verrier, in his tables of the Sun. (41, p. 102.) 2994790 1876. Powai.ky, from observations of the Sun made at Dorpat. (181, p. 265.) 2876000 1876. Le Verrier, in his tables of Jupiter. (8, T. 12, p. 9.) 2812526 1878. A. Hall, from his own observations of the elongations of the satellites. (158, p. 37.) 3093500^:3295 Reciprocals of the mass of Jupiter. 1726. Newton, from the elongations of the fourth satellite, observed by Pound. (9, lib. 3, prop. 8, cor. 2.) . 1 067 1782. La Grange, from a recomputation of the same observations. (167^.183.) 1067-195 1S02. La Place, from the same observations. (7, T. 3, liv. 6, chap. 6, § 21.) 1067-09 1821. Bouvard, from the perturbations of Saturn. (150, p. ij; compare also 8, T. 12, pp. 67-70.) .... 1070-5 1823. NicoLAi, from the perturbations of Juno. (178, p. 226.) 1053924 1826. ENCKE, from the perturbations of Vesta. (152, p. 267.) 1050-36 1837. Airy, from elongations of the fourth satellite, observed by himself. (143^1.47.) 104677 1842. Bessel, from his heliometer measurements of the elongations of the fourth satellite. (147^.64.) . . 1 047-879 ±0-158 1872. Moller, from the perturbations of Faye's Comet. (175, p. 95.) .... 1 047-788 -|- 0-185 1873. Krueger, from the perturbations of Themis. (165,]). 14.) 1 047558 -J- 0-052 18S1. S< hur, from his heliometer measurements of the elongations of all the four satellites. (186, p. 293.) . 1 047232 -j- 0-246 1888. Haerdtl, from the perturbations of Winni omet. (157, p. 262.) 1 047-175 -J- 0014 ON THE SOLAR PARALLAX AND [TS RELATED CONSTANTS 35 Reciprocals of the moss of Saturn. 1726. Newton, from the elongations of Titan. (9, lib. 3, pro]). S, cor. 2.) 3021 17S2. La Grange, from the elongations of Titan. (167, p. 186.) 3358-40 1802. La Place, from the elongations of Titan. (7, T. 3,liv. 6, chap. 6, | 21.) 3 359-40 1S21. Bouvard, from the perturbations of Jupiter. (150, p. ij.) 3 512 1833. Bessel, from his heliometer measurements of the elongations of Titan. (148^.24.) 3 501-6 -J- 0-78 1S76. LeVerrier, in his tables of Jupiter. (8, T. 12, pp. 9 and 70-72.) 35 1885. A. Hall, from his observations of the elongations of Iaperus. (158^, p. 70.) 1481 0-54 H. STRUVE, from his observations of the elongations of Iapetus and Titan. (187 >2, pp. 1 17-1 18.) . 3498-0 | 1.17 1889. A. Hall, Jr., from his heliometer measurements of the elongations of Titan. (161, p. 146.) .... 3 500-5 ± 1 h Reciprocals of the mass of Uranus. 1789. WURM, from IIf.rschel's measurements of the elongations of the exterior satellite. ( 190, p. 214.) . . 16 959 1S02. La Place, from the same observations. (7, T. 3, liv. 6, chap. 6, \ 21.) '9504 1821. Bouvard, in his Tables astronomiqa.es. (150, p. ij.) 17 918 183S. Lamont, from his measurements of the elongations of the second and fourth satellites. ( 168, p. 59.) . 24 605 1871. Von ASTEN, from elongations of Obcron and Titania, observed by Lamont, O. Struve, Lassell, and Marth. (144, p. 21.) 22 1875. Lord Rosse and Dr. CoPELAND, from their observations of Oberon and Titania. (1S2, p. 304.) . . . 24000 1875. Newcomr, from his observations of the elongations of all the four satellite. 1 . 1 ;>•, p. ?6.) 22 540 -j- 50 1885. A. Hall, from his observations of the elongations of Oberon and Titania. (159, p. 33.) 22 682 -j- 27 Reciprocals of the mass of Neptune. 1847. O. Struve, from his own observations of the satellite. (188, p. 815.) 14 494 1848. B. Peirce, from the perturbations of Uranus. (179^.205.) 20000 1849. HlND, from elongations of the satellite, measured by BOND, Lassiii, ami ( ). STRUVE. (l63,p. 203.) 17 900 1850. G. P. Bond, from elongations of the satellite, observed at Cambridge, Mass. (149, p. 3S.) 19400 1854. Hind, from elongations of the satellite, observed by Lassell in 1S52. (164^.47.) 17 135 1S62. Saffok I), from the perturbations of Uranus. (lS5,p. 144.) 20 039 -j- 295 1875. Newtumi'., from his own observations of the elongations of the satellite. (176, p. 63.) 19 380 -L_ 70 1885. A. Hall, from the elongations of the satellite (160, p. 26) : (a) From his own observations 19 092 -}- 64 (6) From Holden's observations 18279-^ 114 (c) From Lassell and Marth's observations 17 850 -L. 180 The various values given above for the masses of Mercury and Venus differ so largely among themselves that no trustworthy result can be deduced from them, and a rediscussion of the original data seems the only satisfactory course. For the masses of the planets outside the Earth the following numbers will be adopted: Mass of Mars zz Oo2) 3 093 500 Jupiter = (io3) 1 047-55 Saturn = ( 1 04) 3 501 -6 Uranus — - O05) 22 600 Neptune =— — — — (106) r 18780 Number (102) is Professor Hall's value. For the mass of Jupiter the arithmeti- cal mean of the values given by Bessel, Moller, Kruegek, Schur, and Haerdtl is 1 : 1 047*522, while the mean of the two values given by Bessel and Schur is 1 : 1 047-555. Number (103) is sensibly the latter value. According to II. Struve,* * 187^, pp. nS-119. ■>6 ON THE SOLAR PARALLAX ANT) ITS RELATED CONSTANTS. the revised value of Bessel's mass of Saturn is 1:3 5025. The mean of that, and the value found by Mr. A. Hall, Jr., is 1:3 5015, which differs so little from Ves- sel's own value that the latter has been retained in (104). Number (105) is very nearlv the arithmetical mean of the values given by Newcomb and Hall, and (106) is almost the arithmetical mean of the values given by Bond, Newcomb, and Hall, the latter including the observations by Holden, Lassell, and Marth. We now proceed to determine the masses of Mercury, Venus, and the Earth from the perturbations, both periodic and secular, of these planets and of Mars. To facili- tate the discussion of the motions of the nodes of Mercury and Venus, let Q, =. longitude of the planet's ascending node, Qo = approximate value of &, such that Q, rr Q,0 + -dQ,, m rr mass of the planet, m0 z= approximate value of m, such that m rr m0( 1 -f- v), i z=. inclination of the planet's orbit to the plane of the ecliptic, tzz time in Julian years of 365^ days, counted from a specified epoch, (/A© rr correction to the assumed value of the Sun's longitude, rffi© = correction to the assumed value of the Sun's latitude, di — correction to the assumed value of ?', dp and 6q zz certain coefficients whose numerical values are given by Le Verrier in the Annales of the Paris Observatory, Tome 2, pp. 100-102. Further, let symbols relating to the different planets be distinguished by superior Roman numerals, in the usual way, those relating to Mercury being without any numeral, while those which relate to Venus are marked ', those which relate to the Earth u, and so on to Neptune, symbols relating to which will be distinguished by the numeral vu. In order to make use of Professor Newcomb's investigation of the longitude of the node of Mercury, let us put 0, — Qo + ^Q, (107) where the value of &0 is that given by Le Verrier for the epoch 1 850*0, in his tables of Mercury,* namely, £0 = 46° 33' 0875" + 42-643"* + 0-000083 5"t2 (108) From a discussion of 23 transits of Mercury, occurring between the years 1677 and 1 88 1, Newcomb found for the epoch i820'ot N — N0 + Wt - - o- 1 6" ± o- 1 8" + (0-28" ± 0-42")* Whence, for the epoch 18500 N==-o-i6//±o-i8" + (o-28"±o-42")-i?52zl^?+(o-28//±o-42,/)< — _ 0-076" ± 0-220" + (0-28" ± O.42")* Newcomb wrote N = (£0 — Perturbations of Venus in latitude Encke's observed Q,' . . . Correction for i/'/.Q . . . . Correction for Correction for perturbations Corrected Q'1 . . . . Transit of 1 76 1. // + 2-45 — 0-07 + 5-64 -|- 0-060 Transit of 1769. // + o-4S + 004 + 5'94 + 0-084 o / // 74 3i 5446 + 245 -f 1-182 + 1765 + 1013 74 32 00 87 o / // 74 36 08-60 + °-45 — 0-675 — 2-014 + I-4I8 74 36 07-78 The provisional expression for the longitude of the node of Venus, employed by Hill in the construction of his tables of that planet, was Q,i=75° 19' 52-3" 4- 32-293 i"£ + o-oooi 51 *2 where t is reckoned in Julian years from the epoch 1850*0. To this, from the meridian observations made at Greenwich, Paris, and Washington during the years 1836 to 1871, he found the correction* sin 1 C059 18 which belongs to the epoch 1855, January 00, Washington mean time. Whence, for that epoch, 81 = 75° 22' 3578" From the 1475 photographs of the last transit of Venus, reduced by the United States Transit of Venus Commission, we have for the epoch 1882, December 6d 5b o'", Greenwich mean time, #=75° 37' 33'9ii" +^A 0-16-868^©- 0-321 di{ This result already depends upon the position of the Sun given in the Tables du Soleil of Hansen and Olufsen, and it requires correction only for the perturbations of Venus in latitude. According to Hill's tables of Venus, these perturbations amount to -f- 0-046", and the corrected result is, therefore, Si = 75° 37' 34W *l62, Introduction, p. 36. ON [TIE SOLAR PARALLAX AND US RELAT1 U CONSTANTS. From Hill's tables of Venus, Introduction, p. 2, we have 39 Gs = 75° *9' 53,io" + 32'5i5o"/ + o-oooi5i//<2 where £=r(I)ate in Washington mean time)— 1850-0 = (I)ate in Greenwich mean time) — i850'000 586 Computing the values of £l for the dates of observation by this expression, and collecting our observed results, we have Julian date. Computed Q' Observed &'• C — O 0 / // 0 / // // 1761-398967 74 31 54'49 74 32 00-87 -6-38 1769392654 74 36 J4'20 74 36 °778 + 642 1854-966 363 75 22 35-66 75 22 35-78 — 0-12 1882-897 900 75 37 4401 75 37 34-69 + 932 In order to form the observation equations for the determination of the corrected expression for &\ let 0=75° 19' 53-10" +£ + (32-51 50" + //)<+o-oooi 51 *2 — (observed Q? at the time t) (in) and then, by putting C for the computed, and O for the corresponding observed value of Q,', we shall have o = (C — 0)-f x + ty The scale of the Julian dates given above is such that 1849-967042 corresponds to 18500 Washington mean time. Bearing that in mind, the following observation equations result from the values of (C — O) : ozr — 6-38 + 3: — 88-568?/ 0 = 4-6-42 +£ — 80-574// 0 = — OT2+.r + 4-999// 0 = + 932+.r +32-93 I// Weight 1 Weight 1 Weight 1 Weight 4 The probable error of the observed right ascension of Venus was +0470'' in 1761, ±0-496" in 1769, and only ±0038" in 1882 Therefore, according to theory the weight of the last observation equation would be more than 150 times that of either of the first two. Nevertheless, on account of the possible existence of constant errors, it has been thought prudent to give it a weight of only four. (112) 4o ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. Having- regard to the adopted weights, the normal equations are o = + 37-200"+ 7'ooox— 32-4193/ 0 = T 1274-847" — 32-4I9Z+ 18699-253// and the general solution is x = — 0-144013 468 P — o-ooo 249 677 Q y = — o-ooo 249 677P — 0-000053 91 1 Q in which P = + 37-200" Q = + 1274-847" From the general solution x — — 5675 601" ± i'973" V = — 0-078016 2" ±0*038 2" with which values the residuals in the normal equations are respectively 00000" and — 00004", while those in the weighted observation equations are respectively — 5'i46," + 7030", —6- 1 86", and +2-151". If it is desired to use only the data afforded by transits of Venus, we may take J (1 76 1 + 1769) and 1882. In that way dp, the unknown correction to the adopted value of the Sun's semi-diameter, is sensibly eliminated from the observations of 1761 and 1769, and our observation equations become o = + 0-02" +# — 84-571?/ o = + 9-32" +£ + 32 93 1 # Whence x = — 6-714" y — — 0-079 147 The difference between this result and that from the normal equations ^112) is less than the probable error of either. Reverting to the values of x and y yielded by the equations (112), and substi- tuting them in (in), we obtain definitively for Venus S1 =75° 19' 47-42" ±r97" + (32-4370" ±00382")* + 0-000151"^ (113) which belongs to the epoch 18500 Washington mean time. If we put with Le Verrier* p — tan i sin Q, q = tan i cos & then, regarding all the quantities as variable, and differentiating dp = ,. di + tan i cos Q-dQ COS' 1 dq = - , . cji _ tan i sin 0,'dQ, cos- 1 *8, T. 2, p. 26. ON THE SOLAR PARALLAX AND lis RELAT] I- CONSTAN 41 whence, by eliminating di, we find for the theoretical motion of the node on the fixed ecliptic dQ rz coti cos Q-dp — cot I sin Q-t/q To find the theoretical motion on the movable ecliptic, it is only necessary to substitute dp — dp" and dq — dqli for dp and dq. In that way wo obtain lor Mercury and Venus dQ, — cot i cos Q {dp — dp") — cot i sin Q (dq — dqa) (114) dQ} = cot il cos S1 (dp1 — dp") — cot i1 sin Q' (dq[ — dqli) (115) From equations (no) and (113), and from Le Vereier's tables of Mercury and Hill's tables of Venus, we have for the epoch 18500 Q =46° 33' 08-13" i -70 00' 0771 a' =75° 19' 47-42" i;=3° 23' 35-oi By the substitution of these values, and after replacing dp, dp\ dp", dq, dq\ and dq" by the numerical values of dp, dp\ dpu, dq, dq\ and dq*, from the Annates of the Paris Observatory, T. 2, pp. 100-101, equations (114) and (115) become (l?=— 7-60689"— 0-065 oo'V —4-102 14' V1 — 0-923 46' VH ' — o-i 12 38'Vm— 2-283 53'Viv— 011704"^ — o-ooi 84'Vvi dO} ,. =- i7,367 93" + 0-11193" v - 5-038 55'V -6-71749"^ (Il6) — 0-22172 Km— 5-22275 f"'— 0-27355 — 0-004 i8"v Putting ^ for the general precession, the observation equations for determining the masses of Mercury, Venus, and the Earth will be of the form o = theoretical -p -4- fa — observed — p (117) dt ill As the masses of all the planets outside the Earth's orbit are here regarded as known, the numerical values of their vs must be substituted in the observation equa- tions. To find them, we have the relation m = »i0( 1 -f- v) where w0 is the value employed in the observation equations for the mass of any planet. or, in other words, it is the value employed by Le Verrier in forming the quantities dp, dq, etc., and m is the adopted mass of the same planet. The numerical values of 1 -^ w0, 1 •— m and v are given for each planet in Table III. 42 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. Table III. Planet. I -r- m% Le Verrier. I -f- m Adopted. Factor V Earth 3 ooo ooo 401 847 354 936 2 680 337 1 050 3 512 24 000 14 400 Indeterminate . . Indeterminate . . Indeterminate . . 3 093 5O0 1 04755 3 501-6 22 600 18780 — 0-I33 558 + 0-002 339 -)- 0-002 97O -)- 0-061 947 — 0233 227 Taking the observed values of the motions of the nodes from equations (1 10) and (113), the theoretical values from the equations (116), and the factors for the correc- tions of the masses from Table III, the formation of the absolute terms of the observa- tion equations will be as follows : Mercury. Venus. Provisional motion of node . Correction for mass of Mars . Correction for mass of Jupiter Correction for mass of Saturn rr — 7-606 89 -j- 0015 01 — 0005 34 — OOOO 35 + 50237 19 rr — I7-367 93 — 0-029 61 — 0-012 21 — OOOO 8l + 50237 19 Theoretical dQ,/dt .... + 42-639 62 -j- 42666 O + 32885 85 + 32-437 © Observed dQ/dt (C — 0) = absolute term . . — 0-026 4 + 0-448 9 The observation equations are therefore // // // // // Ozz — OO659 v — 4-1021 v1 — 09235 vn — 0*0264 zh 0*034 O = + O" I I 1 9 v — 5-0386 vx — 67 1 75 v" + 0*4489 ± 0-038 whence, leaving vh indeterminate, (118) v — + 28-951 626^— 2-495 943 ±0-427 v% — — 0-690 234 vil -f- 0-033 66 1 ± 0005 75 If we assume vn zz + 0*066 631, then v — — 0-566 867 ± 0-427 vl = — coi 2 330 ± 0005 75 In the Annales of the Paris Observatory, T. 6, pp 286 and 307, Le has given four equations which may be used for determining the masses of Vekrier Mercury, ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS 43 Venus, and the Earth. They are derived respectively from tin- secular motions of the perihelion, eccentricity, inclination, and node of .Mars; and, alter multiplication by 100, they are as follows: (119) o = + o-i4v-f 4*66 k'+ 16-36 ku+ 1306 k1*— 2*353 o = + ooSk + 0*69 v[ -\- 2-o6k"-|- iS-2 k1v — 11 15 o = — oiok+ 1222 »''+ C03 y" — 131 1 vlv + 0565 o = — 0*69 v — 25-60^— 6-821'"— 37 15 viv — 0-577 Regarding v, v\ and v" as unknown, the normal equations are // // // " . " 0 = + 05121 k + 1 7-1496 vl-\- 7-i58oKn+ 466845 y'v — 0-0770 0 = + 17-1496^ + 826-8801 ^+252-6176^'+ 141 1-9898 k'v 4- 9-9411 (120) 0 = + 7-1580^ + 252-6 1 76 ^ + 318-4065^ + 24270777 i'iv — 36-8399 and the general solution is v z=—7-o84 439P +0129 718Q + 0-056 347 7 Ii \ov' — + 1-297 176P — 0-039 714Q + 0002 347 2R 100 y" — + 5634 770P + 0-023 472 Q — o 459 359 4^ in which P = + 46-6845 Kiv— 00770 Q = + 1411-9898^+ 9'94n R — + 242 7-0777 vw — 36-8399 By substituting the value of viY from Table III these quantities become P = + o-032i Q=:+ 13-2423 R = — 31-1654 and them from the general solution, v — — 0265 744 ± 1-511 v1 — — o 055 742 ± 0-035 76 v" — + 014S07S + 0-03847 With these values of the ks, the residuals in the normal equations (120) are + 0000001" +0-000055" —0000008" the residuals in the observation equations (119s) are + 00779" —0-8272" — 0-1159" —00634" and the probable error of any one of the observation equations (119) is =1=0-5675". We have next to deal with the following- group of equations : 0=: o'oo>' + 29/-5 ^ + 225-3 v"— 18-59 o = — 2 7-39" -46-33 yi~ 51'59>/ii— l8'°2 o=:+i4-3 " + 25-5 v* + 277 "" + 17 o-+ 7-8 k+ 9-2 V + 153 ^+ 37 C121) O — — 0-53^ + 24-6 v1 + 32.8 va— 186 O — — I-24V + 40-4 VJ + 54-0 Vil— 3-28 o — + 0-53^ + 28-88^ o-o v"+ 174 44 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. When Mais made its near approach to tf1 Aquarii on October i, 1672, the position of the planet was compared with that of the star by Richer at Cayenne, by Picard near Beaufort, and by Roemer at Paris. From a very careful discussion of these compari- sons, Le Verrier derived the equation which he has given in the Comptes Rendus, T. 75, p. 169, namely, o = + 29-5" vx + 225-3" v" + l39%" yiv—2i -86" By substituting in it the value of vivfroni Table III, the first equation of the group (121) results. The second equation of the group (121) is from the Annales of the Paris Observ- atory, T. 6, p. 72>'i ana" is based upon the longitude of Venus deduced from Horrox's observation of the transit of that planet in December, 1639. The third and fourth equations are from the Annales, T. 6, p. 76; the former being derived from the lon- gitudes of Venus obtained from Bradley's meridian observations, and the latter from the longitudes obtained from the meridian observations made between the years 1 766 and 1830. The fifth and sixth equations are from the Annales, T. 6, p. 90; the former being derived from the latitudes of Venus resulting from the observations of the tran- sits in 1 76 1 and 1769, and the latter from the latitudes resulting from the Greenwich meridian observations made between the years 1751 and 1830. In the Annales of the Paris Observatory, T. 4, p. 52, Le Verrier has given the equation oz + 0-53" v + 28-88' V + 0-83" vm + 1 -8 1" (122) which he has derived from the secular diminution of the obliquity of the ecliptic. By adding the term + i6-oi'Vv, from p. 51 of the Annales, and substituting the values of vhi and v** from Table III, the last equation of the group (121) results. In the Annales, T. 5, p. 100, and T. 6, p. 91, and in the Comptes Rendus, T. 75, p. 168, Le Verrier has given equation (122) in the form o = + 0-53" v + 28-88" v1 + 0-75" vm + 1-72" (123) but the difference arises solely from the circumstance that in (122) the assumed mass of Mars is 1 : 2 680337, while in (123) it is 1:2 994 790. For further comments on the equations (121), Tisserand's paper in the Comptes Rendus may be consulted.* From the group of observation equations (121) the following normals result: o o o + 1017-641' 4- 1 657-55 ^+ 1844-16^+ 552-713 + l657'55,/+ 6822-98 k'+ 12 872-101'"+ 235-835 + 1 844-16 v -\- 12 872- 10^+ 58 414-841'" — 3 393-103 (124) 189. ON III1. SOLAR PARALLAX VND ITS RELATED CONS! VNTS. 45 and their general solution is 1 000 v — — 1 764489 702 P + 0553 787 566Q —0066325 742 R 1 000 ^ = + 0-553 7%7 566P — 0-424651 923Q +0-076091 780 I { 1 000 k" — — 0-066 325 742 P + 0076091 780Q —0031 792 362 R where P=r + 552713 Q = + 235-835 R = - 3 393'I03 We therefore have v — — 0619 603 8 + 0-096 92 vl = — 0-052 2494 + OO4755 v" = + 0-089 1 60 8 + orj 1 3 o 1 with which the residuals in the normal equations (124) are + o-ooo 2" + o-ooo 8" + 0-002 8" The residuals in tne observation equations (121) are — 0-043" —6-022" +0-107" —0-097" — 3*228" —0-250" +0-192" and the probable error of any one of the observation equations (121) is + 2-307". The equations in group (125) are from the Annales of the Paris Observatory, T. 4i P- 95> and depend entirely upon observations of the Sun. The first equation of the group has been deduced from the differences of the maximum values of the equation of the center determined at two epochs fifty years apart. The second equation arises from the observed motion of the Earth's perigee; and the remaining equations are based upon the periodic perturbations of the Earth, the third and fifth arising from the action of Venus, while the fourth and sixth arise from the action of Mars. // // // // 0 = — 0*23 v + roi y' — C65 vm — o*2i o = — o 43 v + 5-97 vi + 1 93 vni — o 44 0 = — 004^+ S-oo^1 — 013 vm — 001 (12O O rr + 002 v + r -07 k1 + 4-00 v1" + 0-48 O = — 002 v + 800 v1 — 0'17 v>u — 009 0 = o*oo v + o-6 1 vi + 4-00 vlu + 0-3 5 In accordance with Le Verrier's estimate of the relative accuracy of these equa- tions,* the second will be given a weight of !,. It then becomes o = — o-i4"v+ 1 -99" k1 + 0-64" vUi — 0-15" (126) *4'> PI>- 95-96- 46 llN' I HI SOLAR PARALLAX AND [TS RELATED CONSTANTS. and, regarding v'" as known, the weighted normal equations are o = + 0-0749" v — 0-9695" v[ + o- 1 485" Kin + o-oS 1 1 " o = -o-9695'V+ 134-4972' V' + 4-937i" ^-0-5835" The general solution is v zz — 14-725 041 P — 0*106 143 Q (127) where v* — — o' 1 06 143 P — 0008 200 Q P = + 0-1485 ^" + 0-081 1 Q = + 4-9371 ^"-0-5835 Hence (128) v zz — 2-710 707 v'" — 1*132266 vl =1 — 0-056 246 v™ — 0-003 824 and the residuals in the normal equations (127) are — o-ooo 00" vm + o*ooo 00" + 0*000 20" vm — o-ooo 09" The substitution in (128) of the value of vm from Table III gives v — — 0*770 229 + 0-317 v* = + 0*003 688 + 0-007 49 with which the residuals in the weighted observation equations (125) and (126) are + 0-058" — 0-120" +0-068" —0-065" — 0-022" —0*l82" and the probable error of any one of these equations is +0082 76". Collecting our results, from the groups of equations ( 1 1 8), ( 1 1 9), ( 1 2 1 ), and (125), the values of v are — 0-566 867 ±0-427 — 0-265 744+1-511 — o-6 1 9 604 ± 0-096 92 — 0-770 229 ±0-317 and the values of vl are — 0-012330 ±0005 75 — 0055 742 ±0035 76 — 0-052 249 ±0-047 55 + 0-003 688 ± 0-007 49 while from the groups of equations (119) and (121) the values of v" are + 0*148078 ±0*03847 + 0089 161 +0013 01 ON THF, SOLAR PARALLAX AND ITS RELATED C0NS1 WIS. 47 Instead of attempting to deduce final values from these results, it will be better to reduce the various groups of equations to ;i uniform standard of weight, and then to solve them all simultaneously. The data for that purpose arc as follows: Equations. Probable error. y/ Weight Group (118) . . Group (119) . . Group (121) . . Group (125) . . ± 0036 ±0-507 1 2-307 ± 00828 io-ooo 0635 01 56 4-35 The weight of the equations in group (1 18) is arbitrarily assumed to be 100, and then the weights for the other groups follow from the probable errors given in the second column. By the application of these weights^ each to its own group of equa- tions, the subjoined system of weighted observation equations is obtained: 0 = — 0*659 v — 0 = 4 n 19 v — o zz + 0*089 v + o z= + 0-05 1 v + Or — 0*064 v 4 0=3 — 0*438 v — o zz o*ooo v 4 0-= — 4*273^ — 0 = 4- 2*23 1 v 4- Ozr + i'2iyv-\- ozz — 0*083 v 4- Or — 0*193 v -\- Orr + 0*083 y + O zz — 1 *000 v + o — — 0609 v -\- Ozz — 0*174 V -\- o — + 0087-^4- ozz — 0*087^4- o = o*ooo v 4- The resulting normal equations 41*021 v} 9-235 k" — 0*264 50-386 v' - 67 1 75 ""44-489 2959^ + 10*389 v" — 1*300 0-438 v1 + 1*308 y" — o'6S 1 7*760 v> 4- o-o 1 9 v" 4-0*339 16*256^' — 4-33i ^ — 0422 4*602 vx 4- 35'147,/ii— 2-900 7*227 v1 — 8*048^—2*811 3*978 k* + 4*321 1^4- 0*265 1-435^-4- 2-387^ + 0*577 3*838^ + 5'I 17 vil — 0*290 6302 vi -\- 8424 vA — 0-512 4-505^ O'OOO vil 4- 0*27 1 4"394*'i o'ooo^" — 0*535 8-656 V1 O'OOOK" — 1*02 2 34*800^- 0*000^-4-0*030 4'654 ^ o-oook*1 — 0*235 34-800 k- o'ooo -'" — 029 1 2-654 vl 0*000 k" — o* 800 are (129) o — + 280773 v — 0*4420 v* — 2 1 *3 1 20 v" 4- 19-8172 o — — 0*4420 v 4- 7265*9429 v- 4- 41 78*6252 yVx — 227*7718 0= — 21*3120^4- 4178*6252 yi-\- 61477642 yli — 394*2509 and their general solution is iook zz — 3*576 684 283 P 4001 1 349 517Q — 0*020 113 276R iook* z= + o*oi 1 349 5 1 7P — 0022 63 1 1 15Q +0*015 421 676R ioo^zz — 0*020 1 13 276 1* 4 0015 421 676 Q — 0*026 81 7 889 R (130) 48 ()N THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. where P = + 19-8172 Qrr — 2277718 Rz= — 3942509 We therefore have v — — 0-655352905^0-06580 v{ — — 0*007 003 642 rb 0-005 235 v" = + o*o66 6 1 7 652 i 0-005 698 with which the residuals in the normal equations (130) are + 0'OOOOOl" +0-000 002" + 0-000 002" The residuals in the weighted observation equations (129) are II — 0*1600 — 0-5908 + 0-1850 — 03664 — 0-4964 + 0-0895 — 0-6868 — 09370 -06835 — 0-6303 — 0-0715 — 0-0998 + 0-327* + 0-0785 — 03246 — 0-3097 + 0-1316 -0-4778 — 08186 and the probable error of any one of the weighted observation equations (129) is ±0-3479". As a final check on the solution, we have the relation [m«] + [aii] v + [bii] yi + [c»] v" — [vv~] =. o which is satisfied thus : // \wn\ +41-91363 [an\v — 1 2-987 26 [&«>> + 1-59523 [c»]ku — 26-26407 Sum + 4*2 57 53 [w] + 4-257 3i Check + 000022 It may be remarked that the weight factors were so chosen as to give a probable error of +: 0-360" for each of the observation equations in the group (129), and the fact that this probable error comes out ±0-348" seems to indicate that the relative weights were sufficiently exact. The 9th and 19th observation equations give the largest residuals, and perhaps it might have been better to omit them, but it is not likely that their retention can have sensibly affected the corrections to the masses. ON THE SOLAR PARALLAX \KD ITS RELATED I NTS. 49 From the solution of the group of equations (129) we now have as the definitive result of this investigation Mass of Mercury = °'^ 6^ ± °-°65 ?o = 3000000 8704559^1724742 Mass of Venus = °'992 996 ±0-005 235 = 1 , . 401 847 404681 ± 2 134 v ° ' Mass of Earth = ro666 ! 8 ± °°°5 69» = J_ 354 936 332 768± 1 77« Or, expressed decimally, Mass of Mercury = o-ooo 000 1 14 882 ± o-ooo 000 02 1 933 Mass of Venus = 0-000002 471 082 -4- o'ooo 000 o 1 3 027 (l32) Mass of Earth = cooo 003 005 097 ± 0000 000 01 6 056 With respect to the data employed in these determinations, transits of Mercury have been used down to 1882, transits of Venus to 1883, meridian observations of Mercury to 1842, meridian observations of Venus to 1871, meridian observations of the Sun to 1850, and meridian observations of Mars to 1858. Since these dates there have accumulated 47 years of meridian observations upon Mercury, 18 years upon Venus, 39 years upon the Sun, and 3 1 years upon Mars ; but to utilize them exhaust- ively for determining' the masses of the three interior planets would necessitate an amount of labor almost equivalent to computing new tables of Mercury, Venus, the Sun, and Mars. Some explanation seems desirable respecting the method of computing the prob- able errors of the planetary masses in (131) and (132). The expressions for these masses are of three forms, which may be written a ± b a , b , >. « = — = -±- (133) m = e±/ (134) ™ = — J-T (J35) Whichever of these forms is employed, it is clear that when the probable error is added to, and subtracted from, the most probable value of the mass, the resulting limit- ing values should be the same. That condition is manifestly fulfilled by the forms (133) and (134), and in order that it maybe fulfilled by the form (135) we must have (a + b)/c=i/(g + h) ^^ and also {a — b)/c— 1 / {g — h) The form (135) is usually derived from (133) by the binomial theorem, thus 1 a\ aJ a a 6987 4 bx~1~c^cb , A 037) 5o ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. all terms of the expansion beyond the second being neglected; and for that reason the formula so obtained is sufficiently exact only when b is small compared with a. To obtain a more general expression, we remark that as the maximum and minimum values of (133) are a + b and a — b we may write 2I1- 2cb a-\-b a — b a2 — b2 and therefore, very approximately «±6_ 1 c c _,_ cb a^ (138) As c/a is not precisely equal to 2\a-{-b a — by formula (138) does not rigorously fulfill the conditions (136), but it is far more exact than (137) when b is not small relatively to a, and as b diminishes the results given by (137) and (138) tend to become identical. By reasoning similar to that employed in deducing formula (138), it is easy to obtain c±/=. / e ^ e2 -P 039) which is required in passing from form (134) to (135). Also, for passing from (135) to (134) 1 _ 1 h y±h 9 g2 — h2 (140) But if h has been derived through the forms (138) or (139), as is usually the case, then according to (133) the probable error is dh^/c, and by expressing that quantity in terms of g and h we find, with all needful accuracy 1 _ lw h2 g±h~rjg^ l J2) (141) ON THE SOLAR PARALLAX AND ITS RELATE! J CONSTANTS. 51 19.— TRIGONOMETRICAL DETERMINATIONS OF THE SOLAR PARALLAX. Observations of Mars, when in opposition to the Sun, and at its least distance from the Earth, constitute one of the oldest trigonometrical methods of determining the solar parallax. There are two ways of making the observations. Either the planet is observed on or near the meridian, at two stations situated respectively, in the northern and southern hemispheres; or it is observed soon after rising, and just before setting, at a single station. The first method will be termed the meridian method, the second the diurnal method. In the meridian method the observations may be made either with a transit circle, or with a micrometer attached to an equa- torial telescope. In the diurnal method they may be made either with an equatorial telescope, or with a heliometer. The values of the solar parallax resulting from some of the most noteworthy attempts by the meridian method are as follows : // 1672. J. D. Cassini (196, p. 114) 95 1751. La Caille (Ephemerides des mouvements celestes depuis 1765 jusqu'cn 1774. Paris. Introduction, p. 1) . . 10-38 1835. Henderson (224, p. 103) 9-028 1836. Taylor (265, p. 71) 9253 1856. Gili.iss and Gould (216, p. eclxxxviij) 8-495 1863. WlNNECKE (269, p. 264) 8-964 1865. E. J. Stone (252, p. 97) 8943 1865. Asaph Hall (217, p. lxiv) 8-842 1867. Newcomb (232, p. 22) 8855 1879. Downing (198, p. 127) 8-960 1881. Eastman (200, p. 41) 8-953 1882. E. J. Stone (264, p. 300) 8-95 The following are some of the results from the diurnal method : * // 1672. J. D. Cassini (196, p. 107) I0-2 1672. Flamstead (209) • IO 1719. Pound and Bradley (219, p. 114, and 243, p. 11 11) IO'S 1857. W. C. Bond (195, p. 53) 8-605 1877. Maxwell Hall (218, p. 121) 8789 1879. Gill (214, p. 163) 8-78 Owing to the comparative nearness of the asteroids, and their small, well-defined disks, it has been thought that the solar parallax might be accurately derived from observations made upon them in the manner just described for Mars. Several attempts in that direction are now in progress, but the following are believed to be all the results hitherto published : // 1875. Gai.ie, from Flora (211, p. 7, and 213, p. 67) SS73 1877. Lord Lindsay and Dr. Gill, from Juno (230, p. 211) The same method has also been applied to Mercury and Venus, but there are great difficulties in the way of obtaining satisfactory results from these planets. Transits of Venus. — Until comparatively recently, astronomers have believed that transits of Venus furnish by far the most accurate means of determining the solar 52 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. parallax. Such transits have been observed by three different methods, namely: (1) by noting the times of contact between the limbs of Venus and the Sun ; (2) by observing the position of Venus upon the Sun's disk with a heliometer ; (3) by photo- graphing the Sun with Venus upon its disk, and subsequently measuring the photo- graphs. Contact Observations. — The following are some of the results for solar parallax obtained by different astronomers from contact observations of the transits of Venus in 1 761, 1769, 1874, and ♦1882: Transit of 1761. // 1763. Hornsby (225, p. 494) 973 1763. Short (250, p. 340) 856 I765. PlNGRE (239, p. 32) IO-IO 1767. Planman (242, p. 127) 849 Transit of 1769. 1769. Euler(203^, p. 518) 8-So 1771. Hornsby (226, p. 579) 878 1771. La Lande (227, p. 798) 862 1771. Maskelyne (12, vol. 1, p. 413) 8723 1772. Lexell (229^, pp. 661 and 672) 863 1772. PlNGRE (24O, p. 419) 880 1772. Planman (5, p. 407) 843 1786. Du Sejour (199, p. 486) 8-851 1814. Delambre (3, T. 1, p. xliv) 8552 1815. Ferrer (208, p. 286) 858 1865. Powalky (244, p. 22) 8832 1868. E. J. Stone (256, p. 264) 891 Transits o/1761 and 1769. 1835. Encke (203, p. 309) 8571 Transit of 1874. , 1877. Airy, from British observations (193, p. 16) 8754 1878. E. J. Stone, from British observations (261, p. 294) 8S84 1878. Tupman, from British observations (267, p. 455) 8846 1881. Puiseux, from French observations (247, p. 487) 893 1881. E. J. Stone, from French observations (263, p. 328) 8-88 Transit of 1882. 1SS7. E. J. Stone, from British observations (251, p. 7) 8832 1887. Cruls, from Brazilian observations (197, p. 1237) 8808 The large differences in the parallaxes obtained by different astronomers from the same observations are due to the circumstance that, as the instants of contact are ren- dered uncertain by the intervention of various disturbing phenomena, many of the observers record two or three different times, corresponding to as many different phases which they endeavor to describe, and thus the resulting parallaxes are influ- enced to a certain extent by the interpretation put upon these descriptions. The interior contacts give better results than the exterior ones, but in any case the prob- able error is large. From 61 selected observations of interior contacts of the transit of 1874, discussed by Colonel Tupman,* the present writer found the probable error ^267, twenty on p. 450 and forty-one on p. 453. *. ON THE SOLAR PARALLAX AND rTS RELATED CONSTANTS. 53 of an observed time of contact to be ±4'59", which corresponds to a probable error -I" ±0-15" in the distance between the centers of the Sun and Venus. Actual errors of from 20 to 30 seconds in the observed times of contacts arc by no means uncommon. Observations with Heliometers. — A few heliometers were used in observing the transits of 1874 and 1882, but until the resulting values of the solar parallax are published the accuracy of their work can not be satisfactorily estimated. Photographic Observations. — For observing the transit of 1874 photography was extensively employed by the English, French, German, and United States parti< but the photoheliographs used by the English and Germans differed radically from those used by the French and Americans. In the subsequent measurement of the pictures the English and Germans failed to obtain satisfactory results, while the Americans, and apparently the French also, succeeded completely: and thus it came about that no photographs of the transit of 1882 were attempted either by the Eng- lish or by the Germans, while the Americans and French took many hundreds. So far as known, the following are the values of the solar parallax yielded by the pho- tographs : Transit of 1874. 1881. Todd, from the United States photographs (266, p. 493) 8-883^0034 1885. Obrecht, from the French daguerreotypes (237, p. 1 121) 8-8l 4:°'°6 Transit of 18S2. 1888. iIarkness, from the United States photographs 88424-0012 It may be well to add that Todd's result depends upon 2 1 3 photographs, Obreciit's upon 82 daguerreotypes, and that of the present writer upon 1475 photographs. The multiplication of the square roots of these numbers by the respective probable errors of the results gives zbo'496", -^ 0*5 44", and ±0*461" for the probable error of a single picture. Discussion of Results. — To facilitate the determination of a definitive value from the foregoing results, they have been re-arranged in Table IV, the construction of which will now be explained. Of the many reductions of the observations of the transits of Venus in 1761 and 1769, all made prior to Excke's time are more or less incomplete, and will therefore be ignored. In dealing with the remaining reductions of contact observations it must be borne in mind that within certain limits the value obtained for the parallax depends upon the meaning attached by the computer to the records made by the various observers, and as these records will frequently bear more than one interpretation, the mean of the conclusions reached by several thoroughly competent computers must generally have a higher degree of probability than the conclusion of any one of them. Accordingly, the numbers entered in Table IV are, for the transits of 1761 and 1769, the mean of the results obtained by Encke, Powalky, and E J. Stone; for the transit of 1874, the mean of the five results obtained by Airy, E. J. Stone, Tupman, and Puiseux; and for the transit of 1882, the mean of the results obtained by E. J. Stone and Cruls, giving the former double weight. 54 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. Table IV. — Values of the Solar Parallax obtained by Trigonometrical Methods. Transits op Venus, contact observations. Transits of 1 76 1 and 1769 Transit of 1 874, English and French observations Transit of 1882, English and Brazilian observations . . . . Transits of Venus, photographic observations. Transit of 1874, United States and French photographs . . . Transit of 1882, United States photographs , Oppositions o/A/ars. Opposition of 1832 : Henderson Taylor Opposition of 1 849-' 50: Gilliss and Gould W. C. Bond Opposition of 1862 : Newcomb Asaph Hall Opposition of 1877: Eastman Gill Maxwell Hall , Oppositions of Asteroids. Flora, in 1873. Galle , Juno, in 1874. Lord Lindsay and Dr. Gill , 8771 8-859 8-824 8-859 8-842 9-028 9-253 8-495 8-605 8855 8842 8-953 8-78 8-789 8-873 8-765 From the photographs of transits of Venus the results given are, for the transit of 1874 the mean of the values found by Todd and Obrecht, giving the former double weight, and for the transit of 1882 the result found by the present writer for the U. S. Transit of Venus Commission. * The early observations of Mars for parallax have been ignored because they were made with insufficient instrumental appliances. With respect to the values entered in Table IV, for the opposition of 1832 there exist only the determinations by Henderson and Taylor, and for the opposition of 1849-50 only the determinations by Gilliss and Gould, and by W. C. Bond. For the opposition of 1862 the results obtained by E. J. Stone and Winnecke rest upon but a small part of the data used by Newcomb, and therefore only the results obtained by Newcomb and A. Hall require consideration. Similarly, for the opposition of 1877 we have to deal only with the results obtained by Eastman, Gill, and M. Hall, because Downing employed a very small part of the data used by Eastman, and E. J. Stone's paper is virtually an indorsement of East- man's result. It is believed that the numbers in Table IV fairly represent all the material now in existence for the trigonometrical determination of the solar parallax. What is the most probable result that can be obtained from them % The arithmetical mean of all the values gives 49 = 8-837" ±0-0614" (142) ON THE SOLAR PARALLAX VND ITS RELATED CONST AN 55 The means of the results from observations of Mars arc, from the oppositions of 1832 and 1849-50, 1> = 8-845" and from the oppositions of 1862 and 1877 p = 8-844" Nevertheless, the four values resulting from the oppositions of 1832 and 1849-50 are so discordant that they should probably be rejected. Doing so, the arithmetical mean of all the other values in Table IV gives o' p- 8-834" db 0-0086" (143) Again, taking the means according to the methods of observation, we obtain // From transits of Venus, contacts |)=:8 8i8 From transits of Venus, photographs _p= 8*850 From Mars j} — 8844 From Asteroids ^-=8*819 and the arithmetical mean is p- 8-833" ±0-0056" (144) Finally, considering only the results which seem most likely to be free from con- stant errors, we have // From photographs of transits of Venus, 1874 . . ^ = 8-859 From photographs of transits of Venus, 1882 . . ^ = 8-842 From Gill's observations of Mars ^ = 8*780 From Galle's observations of Flora p 1=8-873 . From Gill's observations of Juno p = 8-765 and the arithmetical mean is p = 8-824" "± 0-0146" (i45) Except in the magnitude of their probable errors, these four means scarcely differ from each other: but so far as there is any choice among them, well settled principles would lead to the selection of (143), and accordingly that will be adopted. 56 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 20.— GENERAL FORMS OF THE CONDITIONAL EQUATIONS. If I is the length of a simple pendulum which makes one vibration per second of mean solar time, the observed force of gravity will be g—irH (146) Upon the assumption that the Earth attracts as if its entire mass were concen- trated at its center of gravity, its attraction at a point upon its surface in latitude q> will be m'/ay (147) The observed force of gravity is the Earth's attractive force diminished by the resolved value of its centrifugal force. Putting o for the ratio of the centrifugal force to the force of gravity at the geographical latitude g>, we have* 4?r2 N cos q> 4 N cos q> " w ~~~ w where N cos q> is the radius of the Earth at latitude is ag _ 4//« cos

) and the resolved part of that force acting in tlje direction of the vertical is AQCI COS2 q) /on ag cos

=.$, and consequently cos2

'. / E I sin* p where the quantity in brackets is the logarithm of the number which it represents. By attributing proper values to the symbols in equation (154) it may be applied either to the Earth revolving around the Sun or to the Moon revolving around the Earth. In the former case we shall have from (16) and (25) T = 3i 558 i49'3H8 (1 + «) = 0-999998 710 and the substitution of these values in ( 1 54) gives * = [2784 993 2]J(s|eO ('55) 58 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. where $ is expressed in seconds of arc. Of the constants which enter this expres- sion I is the most uncertain, and as it is not trustworthy beyond the fifth significant figure, the logarithmic coefficient in (155) is not trustworthy beyond the fifth decimal place. The Earth's mass is very small compared with that of the Sun, and if in con- formity with custom we take the latter for unity, we may write with all needful accuracy E' —y S + E/_ Further, in (155) the symbol E' refers to the mass of the Earth alone, while the quantity usually called the mass of the Earth is the combined mass of the Earth and Moon, denoted by the symbol E. Bearing in mind that the mass of the Moon is expressed in terms of the Earth's mass as unity, it is evident that F/_E/(i+M)_ E - x _|_ m - 1 + M and therefore when E' is changed into E (155) takes the form ^ = [27849932]^— ^j (156) In order to apply ( 1 54) to the case of the Moon revolving around the Earth we must change the symbol S into M, (1 + «) into (1 + n'), T into T„ and p into P Then, from (39) and (57) T1 = 2 36o59i-5s ( 1 + n') — 1 -ooo 908 743 and by substituting these values we find, after a slight transformation W_ sin3P M — [4*665 070 7 — 10] — sin3 P (157) where, as in (155), the logarithmic term is not trustworthy beyond the fifth place of decimals. I" x 755 D'Alembert determined the Moon's mass from the phenomena of pre- cision and nutation, but to do this with extreme accuracy seems a difficult matter. The most recent attempt is by Mr. E. J. Stone,* who states that his equations include all terms of the third order in the lunar theorv. With some changes of notation, and after restoring the factor cos &>„, they are i1 =:(A«+B;ff)cos coQ (158) $ = C«£ COS OO0 *i87, P- 43- ON THE SOLAR PARALLAX AND lis RELATED CONSTANTS. 59 where u is a constant depending upon the Sun's mean disturbing force, the momenta of inertia of the Earth, and the Earth's angular velocity; and A = i + 3 e,2 2 B=i+3cv-6r 2 C = 2ZfI+3^_5 y>\ fl V 2 2 J (159) As Mr. Stone has not published any details respecting these formulae, it may be well to show how they can be derived. According to Serret* Azzi+3e,2 2 Bzzi+3e22-3!2 (160) Czz P but that geometer has neglected terms of the third order with respect to the inclina- tion and eccentricity of the Moon's orbit, and to restore them we must replace I by (i + ^e22) sin I cos I. Bearing in mind that sin £1 zz ;•', we have sin I cos I zzsin 2QI) cos 2(.]I) zz 2y{\ — ;/2)*(i — 2Y2) — (27 — 473)(i — y2)i — 2y — $y3 — etc. and therefore to take account of all terms of the third order in the equations ( 1 60), it suffices to replace I by (1 + 3 ^(27 — sr5) zz 2;/ + 3Cfy — 5/ (161) and I2 by 4/2. Upon making the substitution the equations (159) result. Reverting to the equations (158), eliminating u and e from them, and introducing the sines of the parallaxes instead of the mean distances, we get M AjSshVj? (C£ - B$) sin3 P But from (154) S sin3_p = E/([2,4ii 704 2 — 10] —sin3 p) which being substituted in (162) gives (C£ - B%) sin3 P (162) e;_ M ""A^([2'4ii 704 2-- 10] -sin:» (163) *83, pp. 303, 313, and 315. 60 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. From (24), (61), (64), and (52) exrrOOi6 771 049 e2z=: 0*054 899 720 y =z 0-044 886 793 M = 0-337815 984 and with these values, from (159) A rz + 1 "ooo 42 1 902 Br-f 0*992 432 024 0^ + 0-265609855 (164) In (163) the term sin3jj is so small that we may safely use the value found by assuming p rr 8-834", and by substituting that, together with the values of A, B, and C from (164), we shall have ^=sin3P} 10 288 642 1— 38442769 S (165) To find the relations existing between |J, ^, and P, we equate the right hand members of (157) and (165), and thus obtain 1 = 1 J 1 — 216 236 65 sin3 P 3757 444 9 — 807 952-64 sin3 P (166) The parallactic inequality of the Moon is given by the expression* sinQ'^F^^X^sinD tj + M «! (167) where D is the mean angular distance of the Moon from the Sun ; and when sin D becomes unity, Q' becomes Q. But «,=<'+*') fli = a(i+x) sin P sin p Whence, with the numerical values of (1 + h') and (1 + u) from (57) and (25) «2 ( r + * )sm p n sin p — 7 s • r> = I OOO Q IO 034 — — £ ay (i+x)sinP y ° sin P (168) Delaunay gives f F v , a2 2423 (169) *52, T. 2, p. 847, eq. 342; S3, p. 37, and 57, p. 36. fS2, T. 2, p. 847, eq. 342, and 53, p. 18. ON THE SOLAR PARALLAX AND [TS RELATED I 0NS1 WIS. 6l But instead of using the rigorous formula (i68), he arranged his numerical computa- tions so as to employ the expression (170) 0 a,- P from which, with # = 875" P = 3 4227// 1 -f y P- 47- -f Strictly speaking, it should be the difference of true longitudes of the Sun and Moon. + 52, T. 2, p. 917, eq. (27). £62, P- IOS- — 1 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 63 The substitution of the mean of (178) and (179) in (177) gives F = 0-991 759 8 P Substituting the mean values thus found in (176), and re-arranging the terms, we obtain * = [4-681 9624- io]PL51+M (i8o) where the logarithm of the numerical coefficient is trustworthy only to five places of decimals. If V is the velocity of light, 9 the light equation, or, in other words, the time required by light to traverse the mean radius of the Earth's orbit, and a the equa- torial semidiameter of the Earth, then whence, with the value of a from (3) p = [?^A48l6] (l82) The mean velocity of the Earth in its orbit is* 2 77T TV(i-0 and if we assume the constant of aberration to be the ratio of that velocity to the velocity of light, then 2 7tr tan « = ™- VTV(i-0 But r zz a/ sin p, whence ^-TVtfar^i'VCi-O Substituting the values of a, T, and ex from (3), (16), and (24) [7-5260362] (l84) Va *2, vol. 1, p. 637. / 64 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 21.— THE LEAST SQUARE ADJUSTMENT. The conditions which must be satisfied by the adjusted quantities are embodied in equations (156), (157). (166), (175), (180), (182), and (184). For convenience of reference they are collected in the group (185), where the quantities within brackets are the logarithms of the numbers which they represent, and although given to six places of decimals they are trustworthy only to five. 1 sin3 P M " [4665 070 70 — 10] — sin3 P i o or o or / E V Vi=2>— [2784 993] (7^^) v2 —p - [5-303 1 25 - 10] PQ — T^j o or v3=p — [4'68i 962— 10] PL * + (185) [8-912482] o or v4=. p — l- o or v^zzp — ye [7526036] o<** = l-gj 1-216236-65 sin3 P > I 3757 444 9 — 807 952-64 sin3 P > If the observed quantities were rigorously exact, their substitution in the con- ditional equations (185) would reduce all the right hand members of the latter to zero ; but in general this will not happen, and instead we shall obtain a series of residuals which may be designated vu v2, v3, etc., as indicated in (185). To make these residuals disappear, a series of corrections to the observed quantities must be determined, such that p=p' + dp P-P' + dP 2» = £' + + [o-3446] v6 dd — — [I*7502] (l'4—Vi) — [43242] f5 -\- [4-0198 — 10] v, + [2-1072 — 10] rfi dV — — 4-3242 -(-4-0198 — 10 JE — -13705 — 10 -+- 2-1072 — 10 698*3 66 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. Imagining the symbols dp, dP, d^*, etc., in the first column of the equations (189) to be replaced by zeros, the weighted normal equations (190) have been formed in the usual way, but for lack of space on the page their absolute terms are represented by the letters A, B, C, D, whose values are given in (191). o = + A + 36-482 dp— o-i 12 63^^ + 0614 29^ + 14-822 dot. Oz-r + B — 0*11263(^+16*324 (/j? — 0-37844^^ o-ooooofZo: orr + C + 061429^)— 0-37844(7^+2-8612 dQ O'oooooda: Or= + D+ 14-822 dp o-ooooo(/g o-oooooc2$+ 7-2804 da. (190) A = -fo-425oi vx-\- 0-16451 r2 + 0-20082 v3 + 34'340 vh-\- 0*614 291^ B = — o*ooo 953 02 vx + o-ooi 871 5t;2 — 0*113 55 vs— 0*37844^ C = + 0005 197 6 vl — 0*010207 1*2 + o*6 1 9 30 r3 + 2-0640 v6 D*= — 0*13131 v4+ 14-953 v5 The general solution of (190) is dp — — 0*161 962 A — 0-00031 2B + 0-034 731 C + 0*329 735 D d<£ =. — o-ooo 3 1 2 A — o-o6 1 449 B — 0*008 06 1 C + o-ooo 636 D d£ — + 0*034 731 A — 0008061 B — 0*3580270 — 0*070 709 D da = + 0*329 735 A + 0000 636 B — 0-070 709C — 0*808 655 D (190 (192) By first substituting in (192) the values of A, B, C, and D from (191), and then substituting in (189) the resulting values of dp, d&, dQ, and da, we obtain the formulas (193), which are the expressions for the desired corrections to the observed values of p, P, •£, etc., in terms of vu v2, v3, etc. The coefficients in (193) are the logarithms of the numbers which they represent. Formula; Wo. (193). Vl Vl V3 vt t's Vt dp = — 88367 — 10 — 8-4313—10 — 8-0406 — 10 — 86365 — 10 — 9-8002 — 10 — 84423 - 10 dp = — 87873-10 — 8-6474 — 10 + 00065 — 8-6442 — 10 — 98079 — 10 — 01 294 <*£ = — 6-0641 — 10 — 5-9245 — 10 + 7-2840 - ■ 10 — 59217 — 10 — 70806 — 10 + 7-8079- 10 41 = + 8-1109 — 10 + 7-9710—10 — 9-330I - - 10 + 7-9678 — 10 + 9-1315 — 10 — 98540 - 10 dq = — 99939— 10 + 1-1400 + 8-5155- - 10 — 9-7944— 10 — 0-9581 — 9- 8085 - 10 dh = — 8-3146 — 10 + 7-1326 — 10 + 9-3720 - ■ 10 — 8-0203 — IO — 91842 — 10 + 97844- 10 da = + 9-1454—10 + 87401 — 10 + 8-3494 - - 10 + 9-0260 — 10 — 98858 — 10 + 87510- 10 dd = + 05307 + 0-1254 + 97347- - 10 — 17298 + '•5751 + 0*363 dV = + 22446 + 1*8393 + 1-4488 — 17278 — 2S9I9 + 1-8506 dE = + 3-9890—10 — 2-4493 — 10 — 21533- - 10 — 26551 — 10 — 3SI88 — 10 — 2-4038 — 10 For computing the probable errors of the adjusted values of p, P, ;£, etc., we shall need a series of formula3 expressing each of these adjusted values in terms of the originally observed values. As a first step toward finding them we substitute in (193) the values of vlt v2, v3, etc., from (187), and thus obtain the equations (194). ON THE SOLAR TARALLAX AND ITS RELATED CONSTANTS. 67 Equations No. (194). c/5 0 u - Logarithmic coefficients for computing — dp dv 4t *% dq dp dP ,/Q 3 = — 0-252 22" #e = + 0-10638" Whence, by (193) dE = + 0-000000052 007 E + dE = 0-000003 °57 io4 (T97) The value of E given in (195) was obtained from the normal equations (130), and as they must be satisfied with respect to v and v\ the value of k" deducible from the corrected E of (197) must now be introduced in them, and they must be re-solved. Thus new values will be found for the masses of Mercury and Venus, which in their turn will affect the planetary precession, and through it the entire system of corrections by adjustment. To take account of these changes, some subsidiary formulae are needed, which will now be investigated. Reverting to the normal equations (130), if v" is regarded as known their general solution will be ioov r= — 3'56i 599433A — cooo 266658B ioov1 = — o-ooo 216 658 A — 0-013 762 85 2 B where A = + 19-8172"— 21-312 0"^° B = — 227771 8" + 4 178-625 2'V1 We therefore have v — — 0-705 3 1 5 797 + 0-749 994 745 v* ^ = + 0-031 304960 — 0575051 828^" (198) (199) ON THE SOLAR PARALLAX ANU ITS RELATED CONSTANTS. 69 But E + dE = E(i + ya) r" = dE/E (200) and from Table III, E —0*000002 817409 ; whence, by substitution in (199) v — — 0705 3 1 5 80 + 266 200dE y1 — + 0-03 1 304 96 — 204 lojdE (201) As these equations are of the form the equations for correcting the masses of Mercury and Venus will be of the form m + dm — m{\ + « + b.dEi)=z m{i + a)-\- mb.dE (202) where m is the provisional mass of the planet. With m — o"ooo 000 333333 m[ = o-ooo 002 488 509 from Table III, and the values of m(i -\-d) from (132), a comparison of (201) and (202) gives Mass of Mercury = o-ooo 000 1 14 882 + 0-088 733 dE , . Mass of Venus =0000002 471 082 — 0-507 92 2(?E Finally, if instead of the values of v and v1 formerly used, those from (201) are substituted in (76), we shall obtain g = 50-358 6#/- 31 7i6"dE (204) With the value of dE from (197), equation (204) gives g = 50-358 6" — o-oor 6" = 50-3570" (205) which must be used instead of the value given in (195). With it we find v6 — + 0-10666" (206) A repetition of the computation of dE then gives dE — + o-ooo 000 05 2 000 and no further change occurs in |£. With the residuals from (196) and (206) the formulae (193) give dp rz — 0-024 2 78" dE — — cooo 644" dP = — 0-423 53" da=i— 0-012018" rfg = + 0000 155" dd — + 0989 f (207) eZltzr — 0017 253" dV = — 10-855 miles dQ = — 0-498 87" dE = + o-ooo 000 05 2 000 7o ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. The addition of these corrections to the observed values in (195) and (205), and the substitution of the corrected values in the equations (185), lead to a more exact mass of the Moon and a second series of much diminished residuals, namely i/M = 8rio74 #! = — cooo 578" #4 = — 0000058" V2 = + OOOO 02 2" V5 = + 0"000 02 2" #3 — — o-ooo 528" v6=z — 0000353" To reduce these residuals still further they were substituted in the formulas (193), and gave the additional corrections ^ = + 0-000043" rfL = — 0000330" dP — — 0000 038" da — — o-ooo 1 34" d\Y + etc.] (209) The coefficients a, b, c, etc., are given in (194); the primitive probable errors rxi *Vi *'z. etc' a,'e appended to the observed quantities in (195); and q is the ratio r' /r", r' being the probable error found from the corrections by adjustment for a quantity of weight unity, and r" the probable error assumed for such a quantity in equation (188), namely croi. In Table V the columns headed R0 contain the primi- tive probable errors >\, rv, rz, etc., or in other words, the primitive probable errors of p, P, g, etc. ; while the columns headed Ra contain for each of these quantities the numerical value of the coefficient of q in the algorithm (209). Thus the corrected probable error of the observed value of any one of the quantities p, P, ^, etc., will be qR0j and the probable error of its adjusted value will be #Ra. Table V. — Constants required for computing the Probable Errors of the Observed and Adjusted Quantities. X Ro R. X R» R. // // p J- 00086 -J- 0-004024 a 4: 0-OII// 4 0-008 987 p •121 •028 324 6 I-02s 021854 3? •00248 •002 479 V 36 miles 3S-283 % Oil 2 005 983 Q L •35 J- 0-016 ■05S 169 J- 0.013 "3 E , 16056 ^ 10'-' , 42038 ± 10" 72 ON THE SOLAR 1'ARALLA.X AND ITS RELATED CONSTANTS. The value of q used in computing the probable errors given in the second and fourth columns of Table VI was that found above, namely, 1*675 5- From (207) and (208) dE — + crooo 000 05 1 440 which gives, when substituted in (203) Mass of Mercury — 0000 000 1 19 446 , . Mass of Venus zz o*ooo 002 444 954 By comparing the adjusted mass of the Earth in Table VI with Le Vekkier's value in Table III we find ^" = + 0*084875017 ±o-oo2 499 980 (211) and the substitution of that value in (199) gives v = — 0641 659980 . . vK — — 0-017 502 574 These values of v, v\ and vil satisfy the first two of the normal equations (130), and when substituted in the weighted observation equations (129) they leave the fol- lowing residuals : + 0-093 i"± 0*023 1" +0-0026" ±0-087 9" +0-1388" — 1-048 6" ±0 1679" — 0-62 5 8" ±0-020 1" +0-0298" — 0-5271" ±0-0260" —0-869 4" ±0010 8" —0-7827" — 0-6104" ±0*003 3" — 00264" ±0-0060" — 0-467 5" + 0-245 9" iooooo" +0-1304" ±0*012 8" — 0-3723" — 0-2241" ±00108" +o-2i65"±oo2i 1" —0-8443" -0-8465" Taking into account the probable error of v[\ these residuals give +0-385 005" for the probable error of any one of the weighted observation equations (129); whence, with the weights from the general solution (198) Probable error of v — ± 0-072 659 . . Probable error of vi — ± o 004 517 The data employed in this section, the corrections resulting from the least square adjustment, and the corrected values of the quantities investigated, are all brought together in Table VI. In computing the distances of the Sun and Moon from the Earth, the value used for the equatorial radius of the latter body is that given in (3), and the probable errors of the distances have been found from the formula dD — D cot p. arc 1" dp (214) where D is the distance of either the Sun or Moon, p the corresponding horizontal parallax, and dp its probable error. ON THE SOLAR PARALLAX AND IIS RELATED CONSTANTS 73 TABLE VI. — Results for the Epoch lSoO-Q,upon the assumption that the Earth's Flattening is 1 : L'03-47. Quantities. Observed values. Corrections by ad- justment. Adjusted values. // // // // // P 8834 + 0014 41 — 002424 8-809 76 -J- 000674 P 342308 + 020274 — 042357 3 422656 43 + 004746 i1 50-357 0 -|- 0-004 J6 4- 000015 5o-357i5± 000415 1 9-2331 ± 001877 — 001689 9-2l6 21 + 0-01002 Q 125-46 + 05S642 — 049795 1 24-962 05 + OO97 46 L 6-514 -(- 0-02681 — 0000 97 6-5I303± OO2I97 a 20-466 + 0-01843 — 0-012 15 2045385+ OOI506 e 4970s + I-7090I* 4- 0-99094" 49799094+ O36616 V 1S6 347 + 60-318 miles — 11 -009 miles 186335-99 + 591 17 miles E 0-000003005097 J- o-ooo 000 026 902 } +51440 | 0000003056537 + o-ooo 000 007 043 M 0-012315 7 +0000 042 11 Mass of MercuiT = °-358 340^o-072 659 ^ i 3000000 8371937^1770352 Mass of Venus = ggg2497 ±Q-oo4 5i7 = 401 847 Mass of Earth zz^84 8?5 ± 0"002 5°o_ Mass of Moon zz 354 936 1 409 006 i 1 880 1 327 168 ±754 S1197 3 ±0-277 6 Mean distance from Earth to Sun zz 92 793 500 ± 70 993 miles. Mean distance from Earth to Moon zz 238 857 ± 3 -3 12 miles. 23.— ADDITIONAL FORMULA FOR PRECESSION. If we put / + C002 6'VV o,oooo"//Vi + 0-09517" +o-ooio'V + 00564"^ 1 oooooo*2 ( + 00 1 1 3" 7'v + o-ooo 8" vxi (219) *8, T. 2, pp. 55 and 103. fS, T. 2, pp. 93-96 and 100-102. ON THE SOLAR PARALLAX WD ITS RELATED CONSTANTS. 75 Action of Mars. / + 0-38362" +0-0032"?' +0*197 2'V 1 000 000 S.,p" = (1 + ^Hi) J + 0-03 7 o" k" + 0-006 o" v"' + o- 1 3 7 7" "iv ( + 0-002 3'Vv + o-ooo i'Vvl r+ 0-36157" +0-003 8' V +0-0569"^ ] 000000%" =(i+viU)<+ 0-03 26' V" + 0-005 3' Vm + 0-249 2'V (+ 0-013 5'Vv + 0'000 2"v J> *M Action of Jupiter. + 5870 87" + 0-089 3'V +4'939 i""1 1 000 000 <5.,/' { + 0-003 6"^" + 0-142 3'VH + 2-737 4" yiv — 2-055 5'VV + 0-014 5'V- + 2-64680" +o-io6 5"k + 1-292 5'V 1 000000%" = (i -- "iv) <^ — 0-000 5'V1 + 0-1240"^" — 0-426 8' Viv + 1-552 6'VV — 0-009 6' Vvi Action of Saturn. + 0-64359" + 0-004 i'V +0-228 i'V 1 000 000 %/' = ( 1 - - *-v ) -Ti) (* — 1 850) ' + o-o 1 2 44" ^v + o-ooo 08" v™) ^rri73°34/54-6" - 8-790 7" (*- 1850) (22?) — 2480'V — 18 832" v1 — 2 792"^ + 18760"^ — 3 002" vv — 5" Kvi To prevent the possibility of misapprehension, it may be well to state explicitly that the j^s in the equations (227) relate to the values of the masses adopted in the present paper, and not to Le Verrier's values. *8, T. 2, p. 104. ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 77 Reverting to the equations ( 1 58), and bearing in mind that in tlicm the unit of mass is the Earth without the Moon, we have in the first equation of the group M EM S - 1 + M r* __shr V r*~Bm*p whence, by substitution e zz- EM sin3 P (i+M) sin3i> and from the second and third equations (228, AC cos con (229) (230) With the adjusted values of p, P, ^, Q, E, and M from Table VI, and the values of A, B, and C from (164), these formula} give £ zz 2180 260 tfzz 1 7*348 662' (23O Passing now to the analytical formulae for precession and nutation given by Serret in his admirable memoir,* after applying the corrections explained in con- nection with equation (161), putting A = 1 + 3 e? 2 B = i+^e22-6y Czz^(i+^22- \y2) D = --^e2 2 4 E=--^e22-y2 2 4 2 2 and making some transformations, we have, in our own notation a zz (A* + Bne) cos a?0 — ^ b = - (Ah + Bus) (j C0S 2G}° + ^ nexe\ cos co0 2 sinfi)0 2 b zz «#' cot 2 q?0 + * ^gie'i cos oo0 2 /zz - (Ah + B«£) # cos G}0 = -ag P zz a — (#-{- i-") cot ooQ P' zz & — (ag' + r) cot &><, + 99' c°t2 ^o Q =// + ^' Q' =f +r' — ag + -g2 cot g?0 — r' — f+ V cot co0 (232) (233) *Ss, pp. 313, 314. 315. and 32°- j$ ON THE SOLAR TARALLAX AND ITS RELATED CONSTANTS. iff zz at + bt2 + W CO=GD0+ft2 + a ^-Vt+Y't'+W GD1 = GO0 + Qt+Q't2 + n irr , n COS 2 tt>0 . _ V2 . W — -+- ueij — — ° sin Q, — he L. cos ea0 sin 2 & sin GD0 fX (234) (235) — u cos co0 sin 2 O — ue cos oo0 sin 2 (£ (236) m + a wi + « + x — ^ — cos &>0 sin An + «£ , , cos go0 sin A„ wi — xsv m — 73 j y .G zz — «£ C cos gd0 cos & + * £ — sin a>0 cos 2 & + x sin g?0 cos 20 + he— sin go0 cos 2 (£ m -\-a m -\-a (237) The second and third equations of (158) are respectively identical with the first equation of (232), and with the coefficient of cos Q, in (237), that coefficient being the quantity known as the constant of nutation. e\ is the yearly variation of ev In equa- tions (236) and (237) © and (£ denote respectively the mean longitudes of the Sun and Moon, while A0 and A^ denote the mean anomalies of the same bodies. Usually the symbols © and (£ are employed to denote the true longitudes of the Sun and Moon, and on account of the smallness of the terms which they affect, no material error will arise if they are so interpreted in the present case. As the numerical values of the quantities entering formulae (232) to (237) are scattered throughout the preceding pages, they are collected here for convenience of reference : ej^z + 0'016 771 049 g zz + 0*05 2 481" e\z=. — 0^000000424 5 g' zz — 0-466 543" e2=z + 0-054 899 720 r zz + 0-000019 498" M — — 0-33 7 8 1 5 984 / zz + O'ooo 005 662" y— +0-044886 793 co0— 23° 27' 3^'36" 305 2563578 m' - **•&& - 83-996 848 52 27-321 661 16 ° yy * ° iSi == the sidereal motion of the solar perigee in 365^ days zz 1 1-3618" + 0*1375" ==11-4993" according to Hansen*; or 61-6995" — 50-2357" zz 1 1-4638" according to Le VERRiERf. We adopt the mean, namely, + 1 1-4816" zz cooo 055 664 of radius. g/j zz the sidereal motion of the lunar perigee in 365^ days, which is according to HansenJ — -.(<*>— @ — ^1) zz 216 115-2207" — 69 629-3961" — 50-2230" zz+ 146 435-601 6" zz 0-709 939 830 of radius. *54. P» '6. f 41, pp. 102 and 51. % 54, pp. 15 and 1 6. ON THE SOLAR PARALLAX AM) ITS RELATED I ONSTANTS. 79 In (236) and (237) co0 is the true obliquity of the ecliptic at the instant for whirl W iind fl are required, and we should there take oo0 — 230 27 31-36' —0-466 54" (t— 1850)— 0000 000 73" (t — 1 850)3 whence T COS 2ffl, , . ,. n . Lo^^T^7T-— °'234 4742 +0-000004 365 (t— 1850) sin cOq Log. COSQ30 ==9-962 5337+0-000 00O426 (t— 1850) Log. sin a\ — 9599 9792 —0-000002 264 (£— 1850) These numbers must now be substituted in the formulas under consideration, and we shall follow Le Verrier and Serret in first giving the results for luni-solar pre- cession, and for nutation, with i1, n and e retained as symbols. They are " = + [9'962 7169— 10] % + [9-9592345— 10] ne — g l =— [4*290 2802 — IO] H — [4-28461 I7—IO] HE h — — [4-325 3772- 10] g— [1-99106— 10] n (238) /— + [3-067 264 — IO] K + [3-063 782 — IO] tf£ /= + [3-104 547— 10] g 1F= — [9-658 7186 + 0-000004365 (7 — 1850) — 10] ne sin£ + [773809 +0-000000426(7— 1850)— 10] ne sin 2 & — [8-863010 +0-000000426 (/— 1850) — 10] h sin 2 0 — [7-732 19 +0-000000426 (t— 1850) — 10] ne sin 2 (£ + [7-86605 +0000000426 (t — 1850) — 10] h sin A0 + [7-258 65 +0-000000426 (t— 1850) — 10] ne sin Atf /2 — + [9-386 7779 + 0-000000426 {t— 1850) — 10] ne cos& — [7'375 54 — 0-000002 264 (t— 1850) — 10] ne cos 2 & + [8 500455 - cooo 002 264 (t— 1850) — 10] n cos 2 0 + [7-369 63 — cooo 002 264 (t— 1850) — 10] ne cos 2 (£ (239) (240) After substituting the adjusted value of js? from Table VI, and the values of n and e from (231), the formula'. (238) to (240), in connection with (233) to (235), give 1 = 50-236 22" (t— 1850) +o-ooo 1 10 22" (£—1850)2+ F »-„<> , ,,_ < +0-46654" +0-0053"- +02888"^) 13 27^47 J+0.oo83'Viii+o-i6oi"^ + o-oi3i/VMv D y — o-ooo 000 73" (* — 1 850)2 + & 80 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. W-— {17-2382" +o-ooo 173 2" (t — 1850) + { 0*2070" + o*ooo 000 2" (t — 1 850) — { 1-2655" + 0*000001 2" (t — 1850) — { 0-2042" + o*ooo 000 2" (t — 1850) + { 0-1274" + o*ooo 000 1 " (t — 1850) + { 0-0686" + o-ooo 000 1 ' (t — 1850) } sin 9, ^ sin 2& } sin 20 } sin 2d } sin A0 } sin A< (242) fl = -\-\g-2\6 2" + 0000 0090" (t — 1850) I COS& — {0*0898" — O-OOO OOO 5" (t — 1850)} COS 2& , . + {0-5492" — O-OOO 002 q" it— 1850)} COS 2© ^ ^ + {o*o88 6" — o-ooo 000 5" (t— 1850)} cos 2t£ Respecting co0, it is to be remarked that Le Verrier's data* give g?i****z 23 ° 27' 49*804" for the epoch 1810*7, ana" by bringing that up to 1850*0 with our yearly motion, — 0*466 543", the value of go0 given in (241) is obtained. Of course the vs in (241) relate to the masses of the planets adopted in this paper, and not to Le Verrier's masses. It yet remains to deduce from the group of formulae (241) the ten quantities usually employed in computations relating to precession, and these quantities will be given in a shape permitting of their ready reference to any desired equinox and ecliptic. The transformation from one equinox and ecliptic to another might be effected by Hansen's formulae,! but they involve the constants g, [/', r and /, whose values are not always known, and to avoid that difficulty we shall develop formulae involving only the coefficients in equations (234) and (235). If dip /dt is the annual change of rp at the instant tQ, then by (232) and (234) dip cos G?, +— =a dt cos G?0 rP =a^^}(t-t0) + b(t-toy (244) COS 6O0 V 7 V 7 But by (235), which relates to the epoch T, ©, = ®o + QCo - T) + Q'(to - T)2 (245) whence, with sufficient accuracy cos o?! — cos go0 — Q sin Go0(t0 — T) and by substituting that value in (244), the expression for ip given in (273) results. Further, as in the second equation of (234) a>0 is the true obliquity of the ecliptic at the instant T, in order to change the epoch from T to t0 we have only to substitute ^ for go0; and by so doing the expression for a> given in (273) was obtained. *4"> P- 51- t 78, cols. 114, 139, and 154. <>N rHE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 8l The expressions for ^x and cou in (235), are of the form u =A + B(*-T)+C(*-T)2 where dT '-*W2 and consequently, the values which they assume when the origin of time is changed from T to t0 may be found by the algorithm u' ■- A + B(*0 - T) + C(t0 - T)2 + [B + 2 C(t0 - T)] (t - t0) + C(* - t0f The results are given in (274). If A is the planetary precession during the interval (t — t0), ami ^(a^-f-co) — co0 -f- daoQ, then * \—(if>— fa) sec Oo + da>0) ^^ — (if>— ipi) sec w0-\-(ip — Jp^dcoo sec go0 tan co0 But from (273) and (274) xP-tPi = [a- P - (2P + «Q tan ®0)fo-T)] (*-*,) + (&- P')('-*o)2 i(«h + ®) = *>o + Q(f. - T) + QU - T)2 (247) + [£Q + QU-T)](*-*o) + K/+Q0(*--*o)2 whence ^0zzQ(^0-T) + Q'(^o-T)2+[^Q+Q/(^o-T)](^-g + K/+Q')(^-^o)2 (248) and by substituting these values of O — ^1) andda>0in (246), and rejecting all terms above the second order with respect to (t0 — T) and (t — t0), the expression for A given in (273} results. To find m and n we have the well-known formulae But from (273) m _ *+ cos 00 - d* n= ** sin co (249) dt dt at dtp -a-aQ tan co0(t0 - T) + ib{t - Q (If - + sec co0(a - P) - sec a>0(2P' + PQ tan oo0)(t0 - T) dt + 2 sec o?0 \b - P + JQ(a - P) tan «?„](< -f0) go = a>0 + Q(*0 - T) + Q'(/u - T)a +./(/ - to? sin a> - sin g>0 + [Q(*0 - T) + Q'(* - T)2 +./(/ - *0)2] cos co0 coa o - cos «0 - [Q(*0 - T) + Q'(/0 - T)2 +f(t - t0f] sin oo0 *2, VOl. I, p. 607. 6987 6 g2 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. and by substituting' these values in the formulas (249), and rejecting all terms above the second order with respect to (t0 — T) and (t — t0), we find m = + a cos co0 — (« — P) sec ft>0 + [(2P' + PQ tan co0) sec oo0 — 2aQ sin Go0](t0 — T) -)- a sin &>0(Q2 tan co0 — Q')(t0 — T)2 . . _ ( + [2{b - F) + Q(« - P) tan ©0] sec <*>0 ) _ ( — 2&cosft>0 + 2&Q sin &>0(70 — T) ) — af sin cQ0(t — t0f n z= + a sin ft>0 + «Q(cos ft>0 — sin go0 tan Go0)(t0 — T) — rtcosft)0(Q2 tantt»0 — Q')(^0 — T)2 , . + 2?;[sin ft>„ + Q cos co0(t0 — T)](* — 10) + af cos GQ0(t — 10)2 When converted into numbers by means of the coefficients in (241 ), these expres- sions become m = + 46-063 1 5" + o-ooo 277 23" (t0 — 1850) + 0-000000000 1 15" (t0 — 1850)2 + [o-ooo 277 29" —0000000000 192" (t0— i85o)](^ — ^0) (252) — o-ooo 000 000 623" (t — 10)2 n — + 20-04661" — 0-00008481" (t0 — 1850) — 0-000000000 266" (/0— 1850)2 — [0-00008494" —0-000000000443" (t0— iSso)](t—t0) (253) + o-ooo 000 001 435" (t — t0)2 It is, therefore, evident that when neither (t0 — T) nor (t — 10) exceeds a century, all second order terms may be neglected, and the algebraic expressions for m and u may be written as in (273). Expressions for q>" and 0" have already been found from g, gf, r and r', but we have now to deduce them from the coefficients in (234) and (235). For that purpose we shall employ the equations* q>"2 = (<»! — go)2 + A2 sin2 h(G>i + 00) (254) tan (G" + y + hA) = — ^— sin £Oi + <*>) (255) &>! GO The first of these equations may be written >i (&>! — ft>) " 1 \S 1 A2 sin2 i(G), 4- go) )\ q> — — (goy — go) X 1+ 2\ i-r M ( (go, — GOV S whence, expanding by the binomial theorem " / \ A2 sin2 h(GO, + go) , , ,x = — (©! — ©)— 2V i-r ; + etc_ (256) 2(&»! — ft)) *2, vol. I, p. 607. ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 83 If now we put £(<»!+ go) = w0 + dwn A-a-V _(2P: + PQ tana^-T) (257) B=6-P' + £Q(a-P) tana>0 we shall have from (248), (273), and (274) dte0 = Q(*0-T) + £Q(*-*0) + etc. A = see o?0 A(< — t0) + see &>0 B(/ — /,, ) ^ 5 o»1-G,=zQ(t-t0) + 2Q'(t0-T)(t-t0)-(f-Q')(t-t0y (259) Whence, with sufficient accuracy sin ^(&>j -f- &>) — sin oo0 -\- dco0 cos go0 A2 siir i(^ + co) - + tan2 g>0[A2(* + *0)3 + 2AB(* - *0)3] (260) -|- 2 A2 dco0 tan c»0(£ — /0)2 The substitution of (259) and (260) in (256) gives, after rejecting all terms above the second order with respect to (t0 — T) and {t — t0) = - [Q + tan2 oo0{a - P)2/ 2Q](< - tQ) _ (+2Q'+tana70(a-P)2 I (t -T)(t-t^ (26^ ^-tan2^0(«-P)(2P' + PQtana?0)/Qr'° L){* h) (26l) + \ (/- Q') - tan2 co0(a - P)|6 - P' + iQ(a - P) tan a>„]/Q j(* - t0)2 and as the quantities involved are so related that the coefficient of (/„ — T) is known to be exactly twice that of (t — t0)2, (261) naturally takes the form given in (274). Reverting now to (255); after eliminating A by means of the relation* if> — ip! = A COS £(60! -f go) and putting tan {&' + \4> + Jft) — tan (0O" + dd0") = tan 00" + d90" sec2 0O" (262) we have tan 60" +. d90" sec2 6>0" = -^^ tan £(>, + a>) (263) But, from (247) and (259) 0-^x__ «_P_(2P' + «Q tan Q(70 - T) + (b - P')(t - t0) G>! — GO Q\I+f(t0-T)-l^(t-t0)\ "Q" v ° 7 Q Whence, with sufficient accuracy, through an expansion by the binomial theorem ip — ipx a—V ( 2P' + aQ tan®0 2Q'(« — P) ? ,', T>. co1— co Q ( Q ^ ) (26,n *2, VOl. I, p. 607. 84 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. Also, by putting §(col -f go) — go0 -f cIgo0, and taking the value of doo0 from (258) (265) tan £(«»! + ct») zz tan &>„ -f- 0)/Q + 2Q'(a - P)/Q2](V0 - T) + («-P)sec-'^f/o-T) + tano?0[(&-F)/Q + («-P)(/-Q/)/Q2](^-^) ^ + .K«-P)sec2o?0(^-/0) As (262) gives e" = <9o" + d0,"-i(tf + ft) by taking the values of #0" and d90" from (266) and (267), and remembering that to terms of the first order i(* + *i) = *(«+P)(<-'o) we find 9" - e0" tan tt>0 cos2 0O" [2F + «Q tan co0 + 2Q'(a - P)/Q](*0 -T) + (a — P) sec2 a>0 cos2 £0"(£0 — T) -f ta" ^Q08' 9°" \P - P' + (a - P)(/~ Q')/Q](' ~ U) + J[(« - P) se°2 «o cos2 <90" - (a + P)](* - /0) If we had not transformed (255), but had developed (268) instead of G0l — GO G), — GO sin £(g>! + o>) tan £(©! + g?) we would have obtained the slightly more complicated expression tan ooc cos2 9n" 9" - 9'' - Q [2P' + PQ tan coQ + 2Q'(a - P)/Q]& - T) + cos20o,/(«-P)(^o-T) + ^ ^q S' *'" [& - P + *Q(« - P) tan «>, + (a - P)(/-Q')/Q](* -'«> + J[(a - P) cos2 6?0" - (a + P)](*- f0) (269) ON THE SOLAR PARAL1 W AND ITS RELAT] D I ONSTANTS. 85 If M is the longitude of the ascending- node of the mean ecliptic at the time t + dt, reckoned from the equinox of date t, upon the ecliptic of date t, then M = fl" + ^* + * But e" = e0" + *?ft (270) and therefore, with sufficient accuracy M = e0" + 2((°<>r t + ip, (271) As the relation of M to 0" is the same as that of gd1 to go, when the date of the equinox and ecliptic is changed from T to t0 in (270) and (271), we must evidently have „ (272) M =6?0"+|2^-, + ^|[(i0-T) + (<--«0)] and these are the forms adopted in (274); the values of 00" and d90" /dt being taken from (266) and (268). rp =4i-Qtan<»0(;0-T)](*-g+^-f0)2+¥f co = »0 + Q(*0 - T) + QU - T)2 + f(t - t0f + « A - + sec <*>0[a - P - (2F + PQ tan g?0)<70 - T)](* - 10) + sec gj0[6 _ P + iQ(a _ P) tan t»0](< - *0)2 (273) m = + a cos &>0 — (a — P) sec go0 + [(2F + PQ tan a>0) secco0- 2«Q sin g>0< \(t0-T) + (f-f0)} « rr a sin g>0 + 26 sin oo0[(t0 — T) + (t — £„)] ^ =[P + 2P'(/o-T)](/-g + P'(^-g2 + ^ G,1=ffi>0+Q(*0-T) + QU-T)2 + [_Q + 2Q'{t<)-T)](t-t0) + Q'(t-t0Y + n cp" = - [Q + tan2 ©0(a - P)2/ 2Q](* - *0) + 1 (/- Q') - tan2 G,0(a - P)[6 - F + iQ(« - P) tan g>0]/Q } \ 2&-T) (t-te) + (t-t0y} {m) 00"= arc tan [tan oo0(a— P)/Q] A =+t^l^oCOS2^o//[&_F + (r<_p)(/_Q')/Q] + i(« _ P) sec2 oo0 cos2 60" - £(« + P) 6" = 00" + A [2(t0 -T)-(t- 10)] + P(*0 - T) M = 60" + (2 A + P)[a - T) + (* - Q] 86 ON THE SOLAR PARALLAX AND ITS RELATED I I (NSTANTS. By means of the groups of formula' (273) and (274) the entire system of quan- tities used in computing precession can be readily found for any desired equinox and ecliptic when the expressions for tf>, rfv go, and a^ are known for a given equinox and ecliptic. With respect to the notation, it may be well to remark that ip, od, gou ', 0', 0U tc", and 77. Further, T is the epoch for which the constants in the formulae (234) and (235) were originally computed, while t0 is the date of the new equinox and ecliptic to which the precession is to be referred, and t is the date for which the various quantities are required. In (273) and (274) all the angles and circular functions are expressed in parts of radius, and to convert them into seconds of arc it yet remains to introduce the factor arc 1" wherever necessary. By substituting the coefficients from (241) in the formulae (273) and (274), all the following numerical expressions were obtained, except those for the equinox and ecliptic of 1800; such of the formulae as were referred by their authors to equinoxes and ecliptics other than those of 1800 having been reduced to that epoch by means of the formula- (273) and (274), without the introduction of any extraneous factors. Respecting Hansen's formulas, it should be remarked that the values of «o„ and P given in Table VII differ slightly from those in his Tables du Soleil, p. 5; but the P agrees with that in his Tables de la Lune, p. 16. The dates of publication are, for the article in the Astronomische Nachrichten, September, 1852; for the solar tables, 1853; and for the lunar tables, 1857. TABLE VII. — Values given by various Authors for the Coefficients in Vonm/la' (231) and (235); said Values being all re/erred to the Equinox and Ecliptic of L800. Author. La Place. Bessel. Struve and Peters. Hansen. I.F. Verrier. FormuLf (241). Date. 1802. 1826. 1841. 1852. 1856. 1889. a 1 000 J> + 50-290 34" — 0121 79 + 50-378 26" 0-I2I 79 + 50-379 8 " — 0108 4 + 50-355 93" — 010674 + 50368 88" — 0108 81 + 50354 68" 0106 69 1 000 / 23°27/5i-95// + 0009 84 23° 27' 5381" -\- 0-009 84 230 27' 54-22" + 0-007 35 230 27' 54-80" -f 0-007 05 23° 27' 5561" -f 0-007 '9 23° 27' 5480" -j- 0-006 41 P 1 000 P' + 501 1 1 36" + 0122 15 — 50223 50" -(- OI22 15 -f 50241 1 " + 0-1134 -j- 50-222 95" -j- 01 12 07 + 50-224 43" -f- 0-11289 -+- 50225 20" + 011022 Q I 600 Q' — 0521 41" — 0-002 72 - O48395" — 0-002 72 - 0473 8 " — o-ooi 4 — 0467 70" — o-ooi 40 — 047551" — o-ooi 49 — 0466 47" — o-ooo 73 As Dr. Peters's formulae for nutation have been more used than any others, it will suffice to compare our own with them. Accordingly, formulae (242) and (243) have been reduced to the epoch 1800, and are given below, side by side with Dr. Petkks's more elaborate expressions* When extreme accuracy is desired, some of his small terms may advantageously be added to our formulae. Formulas (242) W— — 17-229 5" sin& + 02070 sin 2& — 0204 2 sin 2(£ + o-o68 6 sinAa Dr. Peters. — 1 7-240 5" sin Q, + 0207 3 sin 2& — o-204 1 sin 2(£ + 0067 7 sin(d — r') — 0-0339 sin(2([ — &) + 00125 sin(20 — Q,) — 00261 sin (3d — O + 001 r 5 sin((X + r') + 0-0150 sin(d— 2© + r') + 0-0058 sin(£ + £-0 + 0-005 7 sin (cl — Q, — rr) 4- 0-002 o sin (C — Q> + T") (277) ♦From 109, pp. 170-172. 88 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. — 1-265 6 sin 2© + 0-1274 sin A0 Formulae (243) Q. = + 9-215 8" cos& — 0-0898 COS 2^ + 00886 COS 2(£ + 0-549 3" COS 2© + 0-004 4 sin (2/1' — Q) + o-oo6 1 sin(2(£— 2©) — 0-005 2 sin(3([-20 + r') (277) + 0-005 3 sin (2©— iT) cout',i- + 0*002 6 cosT' + 0*002 O sin 2.T' + 0-002 5 sin (£+2© — r') + 0-002 8 sin(2([-2r/) + 0-002 4 sin (2d — 2&) — 0-002 4 sin (2©— 2&) — 0-002 8 sin (4C - 2J") — 0-003 3 sin (4C - 2©) — 1 269 4 sin 2© + 0-1279 sin'© — T) — 0'02I 3 sin (© + n — 0-005 8 sin(3©-r) — 0*000 5 sin (2© — 2.T) Dr. Peters. + 9 223 1" cosQ, — 00897 cos 2Q> + o'o88 6 cos 2([ + 0-OI8 I COS(2([ — &) — 0-0067 cos (2© — &) + 0-0113 cos (3d — T') — 0-005 ° cos (C + r1) — 0-003 1 COS (([ + £ — f") + 0-0030 cos((£ — £ — T') — o-oo 10 cos (([ — G + r') — 0-0024 cos(2r' — a) + 0-0023 cos (3C— 2© + /"") + OC02 3 sili 7 ' — o-ooo8 cos 2V — O-OO II COS (([ + 2© — r') + 0'OOI 2 cos (4d— 2/"') + 0-0014 cos(4t— 2©) + 0-551 O COS 2© + 0-009 3 cos (o + r) + 0-0027 cos (3© — F) (278) The differential formula? given above will suffice for computing- the precession in all ordinary cases; but if the general formulae should be required, their computation may be greatly facilitated by using the convenient expressions given by Professor Stockwell for the constants which determine the secular inequalities of the nodes and inclinations of the orbits of the eight principal planets of the solar system.* *S4, pp. l6i-l64and 171-176. ON THE SOLAR PARALLAX AND ITS RELATED CONSTAN1 3 89 24.— THE DENSITY, FLATTEN! Nil, AND MOMENTS OF 1NEUTIA OF THE EARTH. In dealing with tlie equations (291), and in discussing the law of density of the interior of the Earth, we shall need the best attainable values of the Earth's mean density, its surface density, and its precessional moment of inertia. The following is believed to be a tolerably complete list of the more important determinations of the Earth's mean density hitherto published: 1778. Maskelyne and Hutton, from measurements of the attraction of the plumb line by the mountain Sche- hallien, in Scotland. (290, p. 783.) 4 % 1798. Cavendish, from the attraction of two leaden balls, each weighing 3484 pounds, the attraction being measured by a torsion balance. (2S0, p. 522.) 5-48 ^ °'39 1811. Playfair, from his own determination of the mass of Schehallien, combined with MASKELYNE and HuTTON's determination of its attractive force. (302, p. 376.) 4'7'3 1812. Hutton, from Maskelyne's measurements of the attractive force of Schehallien, combined with Pi.ay- FAlR's data for its density. (291, p. 64.) 5- 1823. Carlini, from pendulum observations made on Mt. Cenis, and at Bordeaux at the level of the sea. P- 4o) 4'39 1837. Reich, from the attraction of :\ leiden ball, measured by a torsion balance. (271^.98.) 5-438 J- 0-023 1840. Giulio, from Carlini's pendulum observations on Mt. Cenis, after correcting both Carlini's theory and his adopted length of the pendulum at Bordeaux. (287, p. 384.) 4-95 1842. SAIGEY, from the pendulum observations made by Bougl'ER ami La CoND AMINE in Peru, on Chimborazo and at the level of the sea, in 1 737-1 740. (272, parte 2nda, p. 125.) 4-62 1842. Baily, from the attraction of two spheres of lead, each weighing 380-5 pounds, the attraction being meas- ured by a torsion balance. (271, p. ccxlvij.) 5-675^0-004 1851. Reich, from a rediscussion of the experiments which he made in 1837. (310^.389.) 5-484 _[- 0-020 1851. Reich, from the attraction of a leaden ball, measured by a torsion balance during the years 1847-1849 and 1850. (310, p. 418.) S-583±o-oi5 1856. James and Clarke, from the attraction of the plumb line at Arthur's Seat, Scotland. (282, p. 606.) . . 5316 -J- 0054 1856. Airy, from his pendulum experiments in the Harton Collier)-, England. (270, pp. 342 and 355.) . . . 6-566 J- 0-018 1856. HAUGHTON, from Airy's pendulum experiments in the Harton Colliery. (288, p. 51.) 5'4&o 1865. Pechmann, from deviations of the plumb line in the Alps, 4-7, 5-32, and 613; the mean of which is (14, T. 2, p. 380.) 5-38 1878. Cornu and Baille, from measurements, with a torsion balance, of the attraction of a mass of mercury weighing about 26 pounds. (284, p. 699.) 5'5^ 1878. Cornu and Baille, from BAILY's experiments, after correcting a systematic error. (284, p. 702.) . . . 5559 1878. Poynting, by weighing with a delicate balance the attraction of a sphere of lead having a mass of 340 pounds. (305, p. 18.) 5 r'9 =t°i5 1881. Mendenhai.i., from pendulum observations at Tokio, and upon the summit of Fujiyama, in Japan. (299, p. 1 24, and 300, p. 103.) 577 1883. Sterneck, from pendulum experiments made in the mines at Pribram, Bohemia. (314, p. 91. Mr. Sterneck has made similar experiments in other mines, with very anomalous results. For a review of them, see 308, pp. 234-237.) 5'77 1883. Von JOLLY, from the change in the relative weight of two spherical bottles of mercury, each having a mass of il-o pounds, when they were compared, 1st, with both bottles close to the scale pans, and, 2d, with one bottle close to its pan, and the other suspended 68-9 feet lower down. (293, p. 22.) . . . 5-692 -[- 0-068 1889. WlLSING, from the attraction exerted upon a pendulum by two cylindrical masses of iron, each weighing 715 pounds. (322, p. 141.) 5-579 -(-0012 In several instances two or more of the above results rest upon a single set of experiments, the reductions having been made by different methods, and in such cases we have only to consider the one which seems most trustworthy. Alter the applica- 9o ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. tion of that precept, the various results may be classified according to the methods of observation, as follows: i. — Results from the attractions of mountains, measured by the deviations of the plumb line. 1811. Maskelyne, Hutton, and Playfair . . . . 4713 1856. James and Clarke 5*3*6 (279) 1865. Pechmann 5-38 Arithmetical mean 5'T36 2. — Results from the attractions of known masses of metal, measured either by the torsion balance or by the pendulum. • 1798. Cavendish 5-48 1 85 1. Reich, from his experiments in 1837 .... 54.84 185 1. Reich, from his experiments made in 1847-50 5583 ( % \ 1878. Cornu and Baille 5-56 1878. Baily, corrected by Cornu and Baille ■ ■ . 5559 1889. Wilsing 5-579 Arithmetical mean 5-541 3. — Results from comparisons of pendulum observations made at different dis- tances from the center of the Earth; namely, at the sea-level and upon mountains, or at the surface of the Earth and down in mines. 1840. Carlini, corrected by Giulio 495 1842. Bouguer, La Condamine, and Saigey . . . 4-62 1856. Airy 6566 (281) 1 88 1. Mendenhall 577 1883. Sterneck 577 Arithmetical mean 5*535 4. — Results from weighings made with delicate balances of the usual form. 1878. Poynting 5-69 , g s 1883. Von Jolly 5*692 Arithmetical mean 5*691 The arithmetical mean of the 16 values of the density of the Earth given in (279), (280), (281), and (282) is 54.82, but that attributes too much weight to the discordant values in (279) and (281). On account of our utter ignorance respecting the internal constitution of the Earth, it will be safer to base our conclusions solely upon experi- ments of the second and fourth kinds; and if we take the arithmetical mean of the eight values in (280) and (282), we shall have Mean density of the Earth rr 5*578 ± 0*019 ON fHE SOLAR 1'ARAl I \\ AND ITS RELATED < 91 The last four values of (280) are unquestionably the must trustworthy of the whole series, and the arithmetical mean of them alone givea >-■■ Mean density of the Earth = 55 70 ± 0-004 Probably it will be best to take the mean of the eight values in (280) and (282), giving- half weight to the first two in (280) and to those in (282). In that way \v<; find Mean density of the Earth = 5576 ±0016 (283) which will be adopted. It is scarcely necessary to add that the unit of density here employed is that of distilled water at a temperature of 3920 Fahrenheit. As a basis for estimating the surface density of the Earth, we have the following numbers: 1811. Playfair's data give for the mean density of Schehallien, 9 933 X4713-T- 1 7 804 (302, pp. 374 and 376) 2-63 1823. Carlini. from the lithological constitution of Mt. Cenis, estimated its mean density to be (279, p. 39) . . 2-66 1852. Plana found, from Carlint's pendulum experiments, for the mean density of the rocks upon which the plateau of Mt. Cenis rests (301, p. 187) 2-71 1856. Jamfs and Clarke found for the mean density of Arthur's Seat, Scotland (282, p. 603) 2-75 1856. Airy's data give for the crust in the neighborhood of Harton Collier)-, England (270, p. 342) 2-53 1882. STERNECK found for the mean density of the crust over the Pribram mines, Rohemia (313, p. 118) . . . 275 1889. F. W. Clarke found for the mean density of the outer ten .miles of the Earth's crust 2-40 The thanks of the present writer are due to Professor Clarke for his estimate, which was kindly communicated in the appended letter : Washington, D. C, November u, 1889. Dear Prof. Harkness : In rav estimates relative to the abundance of the chemical elements, I have assumed, for definiteness, a layer of the Earth's crust ten miles thick below sea- level. The volume of this, including the ocean and the continents above sea-level, is 1935000000 cubic miles, of which 1633000000 is solid, and 302000000 sea. Hence, by volume, in round numbers we have 85 per cent, rock and 15 per cent, water. The density of the ocean is a trifle under 103. The figure 103, then, maybe taken as near enough for practical purposes. The density of the solid crust is less easy to determine. The greater part of that crust is probably made up of plutonic rocks; and the average specific gravity of about 200 of these, representing a wide range of localities and varieties, is 2 716. In the crust are both heavier and lighter inclusions, and at its surface we have bodies of rather less heavy sedimentary rocks, which range down to a specific gravity of 2-5, or lower. Probably 2-60 or 2-65 would be near enough for the whole solid mass. Now, taking 85 per cent, solid and 15 per cent, liquid, putting the latter at 1-03 density, we get the following data for the mean density of the whole mass : With density of solid crust 2-5 . . 2-2795 With density of solid crust 2-6 . . 23645 With density of solid crust 2-7 . . 24495 92 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS Total difference, 0*17, or about 7-5 per cent, of the lowest value. Probably 2-4, with an uncertainty of 4 per cent., may be assumed as approximately correct. Yours, truly, F. W. Clarke. The arithmetical mean of the first six of the above estimates is 2 6 7, and if we accept that as the mean density of the solid part of the Earth's crust, and assume, in accordance with Professor Clarke's figures, that 0844 of the crust is solid and 01 56 liquid, then the mean density of the crust will be 2-67X0-844+ 1-03 X 0-156= 2-41 which agrees closely with Professor Clarke's own estimate. But we must not forget the many facts which seem to indicate that the Earth's crust is approximately in a state of hydrostatic equilibrium, and lead to the conclusion that it is more dense beneath the ocean than in the continents.* If such is really the case the comparative lightness of the waters of the sea must be at least partially com- pensated for by the increased density of the strata upon which they rest, and the average surface density of the Earth must exceed Professor Clarke's estimate. Our present knowledge is too meager to warrant any very definite conclusion, but as the continental surface density probably lies between 2-40 and 2*72, we may take the mean of these numbers and attribute to it a probable error equal to half their differ- ence. In that way we find Surface density of the Earth = 2-56 ± o-i6 (284) The phenomena of precession and nutation, and certain perturbations of the Moon, enable us to determine two independent functions of the Earth's moments of inertia, from the first of which the Earth's flattening could be found if the distribution of density in its interior were known, while from the second it can be found without that knowledge. In employing the first function Le Gexdre's law of the distribution of density is usually assumed, and we have now to examine the process thus arising, and the result to which it leads. If we put A, B, and C for the three principal moments of inertia of the Earth, A being the least and C the greatest, then the precessional moment of inertia will be (2C — A — B)/2C. Some writers have called this "the terrestrial constant of precession and nutation," or even " the precession constant," but that is certainly objectionable, because these words have long been employed to designate the annual motion of the vernal equinox, and their use for any other purpose can only lead to needless confusion. Serret gives f 2C-A — B_ 2W 2C vn2 where m and n are respectively the sidereal angular velocities of the Earth about the *286^,p. 364. t«3. P-324- ON nil SOLAR PARALLAX AND ITS RELATED CONSTANTS 93 Sun, and about its own axis. Accordingly, with the Julian year as unit of time, and the value of m from page 78 n/m — 366^249 983 2^-A - B 2C w = 6-283 075 94 — 38861 OO7 K (285) or, if A and B are assumed to be equal, and n is expressed in seconds <»l arc C-A C r= 0000 1 88 403 48 u (286) From (230), after substituting the numerical values of its A, B, C, and cos go0 for the epoch 1850*0 « = + 1089640 i;£ — 4-071 361 5$ (287) and by substituting (287) in (286) C-A C — o-ooo 205 292 o^— o-ooo 767 058 7^1 (288) Formula (286) is perfectly general, but (287) and (288) apply rigorously only to the epoch 1850, and consequently $ and ^ must be reduced to that epoch before being employed in them. From (231), u— 17 34866", whence by (286) C-A = 0-003 268 55 = C J 30595 (289) For convenience of reference, some of the values which other investigators have found for n and (C — A)/C are given in Table VIII. That attributed to La Place is what he himself computed, but his values of the precession and nutation constants are respectively 50-261" and 1006" when reduced to 18500, and their substitution in (288) gives a somewhat greater result, namely (C — A)/C =10002 601 61". Bessel Table VIII. — Values of h and (C — A)/ (J according to various Authors. Date. 1799 1818 1830 1 841 1856 1859 1862 1889 Author. La I'i.ai e (7, T. 2, liv. 5, chap. i. \\ 13-14) ! I ( I, ]>. I30) ... Bessel ( i ^, pp. vand xv) C. A. !■'. Peters (109, p. 161) Le Verrier (8, T. 2, p. 174) Serret (83, p. 323) Hansen (55, p. 472) Formulae (231) and (289) 18-312 17-362 «7'323 I7-378 (C-A):C 0-002 596 62 = 1 •002 924 50 = I •OO345O l6=I •OO3 27I I 2 1 •003 263 77 = I OO3274 13=1 •003 272 = I 17349 I 0-00326855 = ! 385" 341-93 289-84 305-7I 306-39 305-42 305-62 305 95 94 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. did not explain how he obtained the result quoted in Table VIII from the Funda- nienta. The precession and nutation constants employed in that work are respectively 50*31 6 14" and 9/648 9", for the epoch of 1850*0, and their substitution in (288) would give (C — A)/C r: 0002 928 28. The Tabulae Regiomontanae contains neither x nor (C — A)/C, but its values of the precession and nutation constants are respectively 5Q'35i 36" and 8*977 97" f°r l850*o, and their substitution in (287) and (288) leads to the values given in Table VIII. Le Verrier gave only h, from which (C — A)/C has been computed by means of formula (286). Taking the polar semi-diameter of the Earth for unity, if we putft for the polar semi-axis of any one of the hypothetical equipotential strata composing the Earth, and p and e for the density and ellipticity of the same stratum, then Clairaut's derived equation may be written* ° = ( v w - 6£)l>™ + <» % + ■ y («*» and from its integration the theoretical relations of the quantities discussed above will result. But in order to effect the integration it is first necessary to express p in terms of b ; or, in other words, the law governing the distribution of density in the interior of the Earth is required. Le Gendre's (commonly called La Place's) law has usually been assumed, and the investigation has been put in various forms by different authors.*! We shall employ the expressions given by Thomson and Tait,"!" viz. (291) C -i-6(/-i)//«92 whore /is the ratio of the Earth's mean density to its surface density; 60 is the ratio of the centrifugal force to gravity, both taken at the equator; and e is the Earth's flattening. These formulae afford the means of deriving e and/ from the observed value of (C — A)/C ; but here we encounter the difficulty that 0 is the real independent varia- ble, and any attempt to change it leads to very complicated algebraic expressions. To avoid them Table IX has been formed, in which the numerical values of all the quantities involved in the equations (291) are exhibited throughout a sufficient range of the argument 0. In deriving e from SGa/2e w© have taken ». = *£= 0003 467 833 = 2-gg^ 09*) where t^— 7424 252 0688, a — 20926 202 feet, /-= 3*251 169 feet, from (3), (13), and (17)- *28l, p. 276 and 321, vol. I, pp. 225, 226. f294, p. 408; 321, vol. 2, p. 117; 7,T. 2,liv. 5, chap. 1, \ 14 and T. 5, liv. n, chap. 2, g 6; io, T. 2, p. 472; 17, p. 235; 24 >£ ; 15 j£, pp. 1 1 1 and 149 ; 13, pp. 83-87 ; 14, Teil 2, p. 487. J II, vol. I, part 2, pp. 407 and 414. /= •3 (I- - 9 cot 6) 5fo _ 2€ /e2 '3(/- 3 0 / c -A_ £ — i^o ON THE SOLAR PARALLAX AND Ms RELATED CONSTANTS. 95 Entering Table IX with the observed value of (C — A)/C from (289), viz, o#oo3 268 60, we find 0=I44'6529° /= 2145 96 £ — OOO3 359 4 — I : 29767 (293) Whence, with the value of the Earth's mean density from (283) Surface density of the Earth z= 5-576/2-146 = 2-598 (294) Table IX.— Numerical Values of the Quantities which enter the Equations (291). -?i8o° - (i / 5 2e t C- C A 1 34° 2338 74 1787 20 2460 73 1 : 283835 = 0-003523 17 I : 28885 1 = 0-003 4'' ' 99 '35 2356 19 1-81356 2 47O 87 I : 285 004 = 0003 508 72 I : 290- 259=: 0-003 445 20 136 373 65 •841 19 •481 22 286- 198 49408 291703 428 14 '37 •391 «o •870 14 •491 79 287-418 479 25 293186 41080 138 408 55 •90048 •502 59 288664 46424 294-708 393 19 '39 •42601 •932 29 513 63 289936 449 04 29627 1 375 29 140 2443 46 196569 2-52490 I : 291237 = 0003 433 63 I : 297-875 = 0003357 n 141 •46091 2-00080 •536 41 292-565 41804 299523 338 64 142 •478 37 •037 75 ■548 18 293922 402 26 301-217 31987 '43 •495 82 •07671 •56021 295310 38627 302-957 30080 144 ■51327 •11785 •572 50 296-727 37009 304746 281 42 '45 253073 2-161 36 2-585 06 I : 298176 = 0-003 353 72 1 : 306586 = 0-003 261 73 146 •548 '8 •207 46 •597 91 299658 337 '4 308-479 241 71 '47 •565 63 •25636 •6ll 05 301 174 32034 310428 221 36 148 58309 ■308 32 624 49 302724 303 34 312-435 20067 149 ■600 54 •363 60 •638 24 304310 28612 314-501 17964 150 2-617 99 2-422 49 265231 1 : 305933 = 0003 268 69 I : 316630 = 0003 158 26 Le Gendbe's law of the distribution of density within the Earth is given by the equation* p = ~ sin-= sin 0 (295) K where p is the density at the distance r from the Earth's center, F and u are constants, and 0 — r/x. Putting/, p\ and & for the surface values of r, p, and 0, and taking r' for unity, we have from (293), (294), and (295) F = p'/sin Q' — 4-490 7 Further, if n is a fraction such that w/ = r, then nr' /k — n6'- and therefore, upon substituting in it the numerical values of F and & , equation (295) takes the form pzz:^9°^ sin (w 144-652 90) (296) n *i 1, vol. i, part 2, p. 404. g6 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. To evaluate p when w becomes zero, (295) must be written P- sin r F « whence, by differentiating- both numerator and denominator, and making r zero, we find for the center of the Earth P = 1 r -cos K K I F u ---e'Y (297) Table X exhibits the values given by formulae (296) and (297) for the density of the Earth at various distances from its center; distilled water at 392° Fahrenheit being taken as unity. TABLE X. — Density of the Interior of the Earth according to Le Gendre's Law. Distance T. , . Density, from center. ' Distance from center. Density. 10 09 0-8 07 o-6 OS 2598 3812 5057 6-292 7473 8-558 04 o-3 0-2 01 OO 9506 10284 10862 11-217 ii-328 Upon comparing the values of the flattening and surface density in (293) and (294) with the corresponding observed values in (4) and (284), viz: € = 0-003 407 5 = I : 293-47 Surface density of the Earth zz 2 56 ± 016 (298) a satisfactory agreement is found only in the case of the surface density. The two values of the flattening differ largely, but our knowledge respecting the figure of the Earth is scarcely sufficient to render it certain that the discordance exceeds the pos- sible effect of errors of observation. Although the value off in (293) does not agree with that derived by General Clarke from his discussion of the great geodetic arcs, it is nevertheless within the limits of the values found from pendulum experiments, as will be evident from an examination of Table XI. ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. Table XL — Flattening of the Earth as found from Pendulum Experiments. 97 Date. 1S30 I.S.U 1842 1853 1S69 1876 18S0 1SS4 1S84 Author. e Airy (17,^231) Ham .y (29, p. 94) BORENEUS (29V, p. l8) Paucker (25^,T. 13, p. 230) UNFERDINGER (39, pp. 313, 324, and 329). A. Fischer (24^, p. 87) Clarke (13, p. 350) Helmert (i4,Teil 2, p. 241) Hill (S7'A> P- 339. foot-note) : I : 28289 I : 285-26 I : 289- I : 28838 i : 29915 I : 284*4 I : 2922 J- 15 I : 29926 -J- 126 I : 285-44 I : 29002 (C — A)/C is certainly much better known than e, and more data for the deter- mination of the latter are greatly needed. Respecting its derivation from pendulum experiments, we may remark that when the length, of the pendulum is expressed by a complicated formula, such as Unferdixger's or Hill's, the simplest procedure will be to compute the numerical length of the pendulum at the equator and at the pole, and then, calling these lengths respectively l0 and Z^, formula (i i) gives 1 S, ioa\ When the pendulum formula gives different lengths at the two poles, different flatten- ings will result for the two hemispheres. Perhaps something might be gained by using Airy's extension of Clairaut's theorem to terms of the second order.* If 4 is the mean density of the Earth; i, p', and e' the values assumed by b, p, and e at the sea-level ; and p — /(6); then it can be shown that after integration (290) must satisfy the following conditions :f I II III IV /(0=P' lbV(b)db c -A £ bY(b)db zxJ 2/(0)-, (i6^,p.562. >)" db db Cry - i<70) 5^0 (299) t320>P-523. €987- q8 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. With our own numerical values from (4), (283), (284), and (292) %4=i 859^0-0053 p' = 2-$6 ±0'i6 C-A 1-9530 (300) f^= 0-39305 Roche,* Lipschitz,! Darwin,}: Tisserand,§ Hill,|| and LevyH have used forms of f(b) other than Le Gendre's law for integrating equation (290), but, singularly enough, when substituted in the left-hand member of IV of (299) they all give very nearly 1 -987, while with the geodetic value of e the right-hand member gives 1 -953. Poincare has recently investigated the subject in a more general manner** and has concluded that no form of /(&) which is continuous between the limits o and 1 can satisfy the observed values of precession and nutation together with General Clarke's value of the flattening. He adds incidentally that the limiting values of the left-hand member of IV of (299) are 1-987 and 2 04 ; whence it follows that the limiting values of £ are 1 : 296 and 1 : 300. We are therefore in this dilemma: Either the flattening must lie between 1 : 296 and 1 : 300, or the distribution of density within the Earth can not be represented by any function which increases continuously from the surface to the center. Those perturbations of the Moon which arise from the figure of the Earth have been discussed by many geometers, among whom La Place, Plana, Pontecoulant, Hansen, and Hill are conspicuous. If we designate the maximum values of the per- turbations in latitude and longitude respectively by <5,s and Sv, then according to HiLLff Ss-/J-,G 6v-ftlB. (301) «2- «,- where 3 3 3 2 3 96 4 4 of 9 nrn J + (r\+y + 6e?+1*?-2 £AL-4f+I3f|3/ (30,) V 4 2 Q xmrn m 18 288 -2oyW-e^-W + ^-S .*,)^ 9 44 "52 4 "* 576 3456 4- 3?925 tf_!9«._ 3449 m_ 59245^2 Hi f 1 38 „ 3 20 , 0.1^2 yip \ 1 = +( +%- r — 7Y — — ye; - 1 9xer + -*- -V77 )— 2 V 3 v 3 9 nrn Jnr (303) *3U. t296and297. £286. £31731^319. H289. ^295. ^303, p. 67. tt57K-PP- 2I3> 308, and 316. ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 99 With the numerical values of m,w", y, eu c,, i/\ and "_./", from (54), (33), (64), (24), (61), (241), (168), and Table VI, (302) and (303) give G = — 1 1977097 II — + 105-29095 (304) Further a(i+*') ^ = 3siu2-(c_A + li) sin P 2E V 2 y and by substituting these values in (301) we have, when A and B are assumed equal, and Ss and Sv are expressed in seconds of arc t, sin2 P sin 201 /ri . . Ss Sv , s -(C-A) = - = — (305) 2EV(i + x')2arci" G "II Whether the Earth was originally fluid or not, for our present purpose it may be regarded as covered by a fluid, because all observations relating to its figure are reduced to the sea-level; and by combining that fact with the single assumption that its interior is composed of nearly spherical strata whose densities are any function whatever of their distances from the center, La Place showed that* 2C — A — B = — 7r(e — i«r0)a2 f prhlr f F" whence, as prdr = — , and A and B are assumed to be equal C-A = 2(e-i«r.)EV (306) By eliminating C — A between (305) and (306), the following expressions result for finding: the flattening of the Earth from the observed values of Ss and Sv : • sin2Psin2GL> , , _ N Ss Sv (a-l*d=- = — (307) (i + «')2arci" G H With the numerical values from Table VI, (57), (7%)i (292), (302) ana* (3°3)> (305) and (307) give C — A = — o-ooo i3444E'«2(5s /,ogx — + 0000 152 93 E' arSv e — + o-ooi 7^3 92 — o-ooo 201 67 Ss (^OQ) — + o-ooi 72)0 92 + °'000 229 4° $v On account of accidental errors in the observed values of Ss and Sv, the two formula' in each of these pairs will seldom yield identical results. To obtain the most *7, T. 3,liv. 7, chap. z,\ 20. -- DEPARTMENT OF PHYSICS Case School ot FipplicD Science CLEVELAND OHIO - IOO ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. probable values of C — A and e we must therefore resort to the method of least squares, and when the probable errors of Ss and Sv are equal, that gives C — A = ( — o-ooo 075 836 Ss + 0000 066 668 Sv)E'a2 £=r + o-oo 1 733 92 — 0000 1 13 75 Ss-\- o-ooo 100 00 Sv ' The formulae (309) are independent of all theories respecting- the distribution of matter within the Earth, Sir Geo. G. Stokes having shown* that equation (306) remains valid, whatever that distribution may be; and, as Dr. Hill has carried the expressions (302) and (303) to terms of the eighth order in the lunar theory, the uncertainty in the coefficients of Ss and Sv is not likely to exceed four or five units in the last place of decimals. For comparison with (309), it will suffice to quote the formulae found respectively by Pontecoulant and Hansen. Those of Pontecoulant are algebraically identical with (307), but his series for G and H are not pushed so far as in (302) and (303), the expressions employed being f G = (_2_w-i§^ + ei* + 4tan'iy-2 V 3 4 18 3 Sm2 tt f . T9 . *3 \tanl V 3 8 y m* With our values of the constants, from (24), (54), and (65), these expressions give G = — 1 2 1448 40 H = + 103*88052 whence, by substitution in (307) £=: + °'001 J2>2> 92 — o*ooo 198 88 Ss r=-|-o-ooi 7 t,t, 92 -f o-ooo 232 51 Sv (3") (312) Hansen's formulae are, in his own notation! ^yi+4 shr-U" a + rj—p p=:£(p — 2( — ) — — ; -A, vL)y sin e cos e 2 + (a + V — i;) ^=20 siniJ^i +|sin21J^i — £0+ T?~ P)~\ Ai His a, 77, and^j are related to our «/', //, and ipu through the expressions «/'(> + -7) = >" »"P = A and as his p, g>, D, J, e, A1} and ttu are our e, ff0, 1\, I, 00, Ss, and Sv, the formulae {312) become in our notation e=^0-i±±^[n2^avcl" . *-** Ss sin2 P sin 100 211I' -\- n — tpx (7,17,) Sv - 20 sin £I(i +^ sin2 £I)[i - h(n — A)/<]Ss 2 *&Vz, p. 680. fio, T. 4, pp. 485-4S6. J5S, pp. 348, 469, and 471. ONTIIESOI.AU PARALLAX AND IIS RELAT1 D CONS! Wis IOI With the numerical values from Table VI, (49), (53), (65), (78), (241) and (292), (313) gives Sv — — 0*898 624.6s £ = + o-ooi 73s 92 — o'ooo 196 62 6s (3*4) = -f o'ooi 733 92 +0000 218 80 ^k The formulae (309) and (311) are directly comparable with each other, but not with (314)- Owing to the peculiar form of Hansen's lunar theory, his perturbations differ from those found in the usual ecliptic .theory, and to avoid the troublesome transformations which occur in passing from the one theory to the other, we shall derive the necessary transition factors by comparing (309) and (314). Distinguishing Hansen's 6s and 6v by accents, and equating the corresponding expressions in the two sets of formula?, we have 201 667 6s •=. 196 61 7 6s' 229 400 6 v = 2 1 8 798 6v' Whence 6s = 0974 96 6s' 6v = 0-953 78 Sv' (315) Table XII contains the values of 6s and 6v determined from observation by various astronomers, together with the resulting values of C — A and e, computed by means of the formulae (308), (309), and (310). The values of 6s and<5^, which Burg originally derived in 1806, and revised in 1823-182 5, are based upon 3233 observa- tions of the Moon, made by Maskelyne, at Greenwich, during the }Tears 1 765 to 1 793 * Burckhardt's values are based upon "more than four thousand observations," which La Place says were those of Bradley and Maskelyne.t Aiey's value is based upon the entire series of lunar observations made at Greenwich during the years 1750 to 1 85 1, in which the data used by Burg and Burckhardt are included, and constitute but a small part. Hansen never explained the derivation of his values, but simply wrote : " Die Mondbeobachtungen haben mir gegeben Ax rr — 8-382", irl — — 7-624", whence the numbers in Table XII result through the formulae (315): // » Table XII. — Observed Values of certain Perturbations of the Moon which depend upon the Figure of the Earth, together with the resulting Values o/O — A and e. Date. 1806 1812 1823 1825 1861 1862 Authority. BLvRO (39 yz, Introduction Tab. de la Lune) Rurckharot (45X> Introduction) . . . 1!'K<; (45K. s. 324) Burg (45^,5.14) Airy (44, p. 12) Hansen (55, p. 470) 6s rr 80 80 86 8172 Sv n 6-8 70 729 6-44 + 7-272 C — A o-ooi 06003 EV- 000 1 073 37 V.'tf- OOOI I38 21' I o-ooo 984 87 Y.'.i'- o-ooi 104 54 I " 0-003 323 92 = 1 : 3°°-85 0-003 343 92 = 1 : 29905 0-003 441 17 = I : 290-60 0003 211 26= I : 31140 0003 390 68 I : 294-93 *45/4.col. 314. t57%> P- 225. La Place was a member of the Commission appointed by the French Bureau of Longitudes to examine Burckhardt's tables, previous to their official adoption. 102 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. Of the results contained in Table XII, those found from the data of Hansen are probably the most trustworthy. Accordingly we shall take C — A = o-ooi 104 54EV (3T6) err 0-003 39068= 1 : 294-93 (317) whence, by comparing (289) and (316) A = 0-336 83 EV C = 0-337 93 EV (318) where E' is the mass of the Earth, and a its equatorial semi-diameter. This method of determining the numerical values of the Earth's moments of inertia is due to Hansen,* who has pointed out that it affords a fine confirmation of the Earth's increase of density from its surface to its center, the value of C for a homo- geneous spheroid being much greater, viz, 0400 00 E'er. 25.— UNCERTAINTY IN THE VALUE OF e, AND ITS EFFECT UPON THE OTHER CONSTANTS. The actual state of our knowledge respecting the flattening of the Earth is best shown by bringing together the more important determinations of that quantity from (4), Table XI, (293) and (3 1 7). They are From geodetic arcs (Clarke) 1 : 293-47 From pendulum experiments (Hill) 1 : 287-71 From pendulum experiments (Clarke) 1:2922 From pendulum experiments (Helmert) 1 : 299-26 From precession and nutation, combined with Le Gendre's law of density . 1 : 297-67 From perturbations of the Moon 1 : 29493 Most unfortunately, every one of these results is affected by much uncertainty. General Clarke used six separate arcs in determining his spheroid of 1880, all of which were well represented by equations (3) and (4). Recently two of the longest of these arcs have been connected, namely, the Anglo-French and the Russian, and according to statements made at the Paris International Geodetic Congress of October, 1889, it now appears that the similar ellipses passing through them have neither a common center nor common axes! Thus General Clarke's e is invalidated, and the possibility of deriving a trustworthy value from the present arcs becomes questionable. The pen- dulum experiments are equally unsatisfactory. The result which Helmert deduced from them by the condensation method, differs largely from that found by Hill through a formula involving twenty unknown quantities, while General Clarke's value, com- puted yet otherwise, agrees with neither Helmert's nor Hill's, but lies midway between them. In 1827 Biot discussed a number of pendulum experiments, which he divided into three groups, having their respective centers as nearly as possible at the *287yz,s.i9s. ON 111!*; SOLAR PARALLAX AND ITS RELATED CONS1 WIS. ' ' »3 equator, at latitude 450, and at the pole. From the first and second groups he found err I : 27638 ; from the second and third, t — 1 : 306*33 ; and from the first and third, e_ r •. 2ox>-59.* These results look as if the flattening varied with the region con- taining the dominating number of pendulum experiments, but it is more probable that their discordance arises from accidental peculiarities of the stations occupied, and there is reason to fear that even yet we have not accumulated sufficient data to eliminate all such peculiarities. As to the result derived from precession and nutation, it is evi- dently vitiated by our ignorance of the internal constitution of the Earth; and even the theoretically exact value from lunar perturbations is rendered questionable by tin- uncertainty attaching to the observed values of the perturbations themselves. Indeed the facts thus far adduced scarcely warrant any conclusion more definite than that the flattening probably lies between 1 : 290 and 1 : 300, but we shall see presently that there is some further evidence which tends in the direction of the smaller limit. We have next to examine how much the system of constants given on page jt, is affected by the uncertainty in the Earth's flattening, and on account of the number of variables involved, the simplest procedure will be to recompute them all with an assumed flattening of 1 : 300. For that purpose the numerical coefficients in formula- (156), (157), and (166) require modification. A comparison of (152) and (156) shows that the logarithmic coefficient of the latter is X\og 4«(i-M)3 4-68557487 = 278499322 (319) Here I, p, and a are functions of e , and when e becomes e + de, I, p, and a become respectively I + dl, p + dp, and a + da. Accordingly, we may write (l + dl){p + dpf [1+ {a + da) V§] lp\i+Gs/%) l + dl (p + dpf w l + gvi and, therefore, A log 4«(i + »)3 -4-68557487 * *(*+rf9(p + #mi+(* + Ar)Vt] 0 (32o) = 2784993 « + ilog^ + ilog— ^— + 41o" >g l + dl J (p + d/o)2 i + 0 + ^)Vg Formula (11) gives for the length of the seconds pendulum at latitude 45 ° li5 = k(i — _0 + *oa/2t{ whence I _^— io«/2*i2 (32i) ° " i-2f - . - - . . - — ■ ' * 20^, P. 38. 104 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. Again, as arc sin V& = 35° 15' 52", the length of the pendulum at that latitude is \oa_c-. ioa\*—fc 10a . . l« = : 4(i - JO + w - (/■ - ^rj rrp + ^7 (322) or, with the numerical values of li5, a and tx from page 9 ?353 = 3'245 629 7 * + 0009 395 4 feet (323) I ££ Differentiating (323), and dropping the subscript 35*3 di_ 3-24563 rf Q-54Q 94 de ,.2.s (U- ecl^io5 (T=^y2^ (324) and then, with sufficient accuracy ri--i-^=i-|°-54Q94de Z + dZ 2 ^1— if) lo». l __ Q-54Q 94 M, where M is the modulus of the common system of logarithms. From (4) and (5) and with that value of e2, and sin 2q> = £, (7) gives Differentiating (325) e2zr2£ — e2 de=z± 1 — (326) 0 1 — as 4- 6e2 — 4«3+ £4 / _v P=- -, „,^ (327) 3 — 2 £ + £ dp = - 6 + 3Q' ~ 44*2 + 28e* - 10^ + 2^ ( g) and then, with sufficient accuracy P2 _ p2 _ _ 2dp (P + de-fl ■ (330) ( 1 — Z > ON Till': SOLAR PARALLAX AND ITS RELATED CONSTANTS. 105 and by substituting the values of dl and de from (324) and (326), together with sin2 cp — £ 106 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. These formulae are adapted to any value of the flattening between the limits i : 290 and 1 : 300, and in order to facilitate their use the following supplementary expressions are added : dezz e — 1/293466 =. £ — o'ocv} 407 55 log (216236648— 106 561 de) = 5-334929300 — 0-214 020 de , . log (3757 444 92 — o-oio 357 de) — 0-574 892 623 — o-ooi 197 de log (807952643— 398 1 57 de) — 5907 385 906 — 0-214021 de With a flattening of 1 : 300, de — — 0*000074 22, and the conditions which must be satisfied by the adjusted quantities are, from (336), (175), (180), (182), and (18 1 sin3 P M [4665 054 83 — 10J — sin3 P o or r, -p- [2784 988] f 7qrjj\ oorv2=p — [5303 125 — io]PQ^^j 0 or v3=p — [4681 962— 10] PL1^"— (338) [8912482] o or t>4 = i> — L yV(^ — J [7-526016] O or i'5 rz « — L— ■ „ ^-J \ « oorP,=i-gj . - 216 244-56 sin3 P> *< 3-757 445 7 — 807 982-20 sin3 P> The values of the observed quantities will be the same as in (195); except those of P and <§, for which (70), (75), and (204) give P = 3 423-08"+ 5062"^ ±0-121" . g= 50-358 6"- 31 716" dE ±0-00248" Uo9; With the above value of de, and d E = + 0000 000 05 1 , we therefore have p — 8-834" ± o-ooS 6" P=r3422704 ±0121 g = 50-3570 + 0-00248 <& = 9-233 1 +001 1 2 Q= 125-46 ±035 ( o) L- 6-514 +0016 ^ ' a — 20-466 +o-Ol 1 6 rr 4970" + ro2s V = 186347 + 36 miles E rr 0*000003 °°5 °97 ±0-000000016056 . ON THE SOLAR PARALLAX AND lis RELATED CONSTANTS. '"7 The substitution of these observed values in the conditional equations (338) leads to the following- system of numbers 1 /M = 81722 6 Vj = + 0-073 81" #4 = + 0007 20" v2 — — 000959 Vry= + 0-029 99 (341) 'V. = — 0033 55 i'c = + 0-035 60 from which the corrections by adjustment given in Table XIII result by a double application of the formula1 (193), precisely as in the case of Table VI. It is now desirable to have a method more direct than that employed on page 72 for finding the probable errors of the masses of Mercury and Venus after they have been corrected on account of dE. As the expressions (203) are of the form A' + B'rfE — (1 + v)/mo, the expressions for v, v\ and v" will be of the form v — A"-|-B"cZE, and when they are substituted in the observation equations (129) the resulting residuals will be of the form, v — A'" + B'VZE. We may therefore write ^y = A + B.rfE + C(dE)2 (342) and if the probable error of dE is =h SE', when that quantity is given there will be an additional term of the form + D(rfE')2. The algebraic expressions for A, B, C and D are simple enough, but they are not needed here because the numerical values of these constants can be most readily found by an indirect process. The residuals on page 48 give 2vv zz 4*257 31 ; those on page 72 give, for rfE = + 5 1 440 =t: 27 33 1, 2w = 5-500 65 + 0-578 55, where 0-578 55 is the part aris- ing from the probable error of dE ; and a special computation gives, for dE zz + 25 000, ■2^ = 4-551 04. In accordance with (342), these numbers yield the equations 4-25731 zzA 5-500 65 zz A + 5-144 o B + 26-460 74 C ^ ^ 4-55 1 04 = A + 2-5000 B+ 6-250 00 C 0-57855 = 7-469840 where rfE andtfE' have been multiplied by 100 000 000 for convenience in printing. The solution of (343) gives ^ = 4-25731 + [3627 3>7E + [14-671 gi](dE)- , . + [14-889 o3](^E')2 V°44; the quantities within brackets being the logarithms of the numbers they represent. From (198), (203), and (344), together with the usual formula for probable error, the following general expressions for the corrected masses of Mercury, Venus and the Earth have been derived : „ „ ,, 0^44647 + 266 200 dE ± R Mass of Mercury zz J- J 3 000 000 Maas of Venus =*196 - «*«>7 an^ from that, together with (350) and (352) i^ + *o (2 — c0) €0= 1/295-5=0-003384095 de=. 10 v arc 1" Vrr 10 348*2 de (353) The substitution of the values of u and v from (351) and (353) in the first equation °f (347) gives db-- 391-6 -9 077 539 de (354) and by differentiating the expression «0(i — e0) = bd, and substituting the values of b0, e0, and db from (348), (353). and (354) da = -^L. -\--Ml^--39r9+ 11 SS9 01 1 de i—e0 ( 1 — £0)- ( Then (348), (353), (354), and (355) give a = b0/(i —e0)-\-da= 20925923-7+ 11 889 on de feet b — b0-\-db =20855108-4— 9077 539 de feet and by changing e0 from 1/295-5 to r/293'47> we obtain finally a — 20926 202 4- 1 1 88901 1 de feet 6 = 20854 895— 9 077 539 df feet (355) (356) ■i.P-3'7- |i3,pp. in and 313. IIO ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. For a flattening of i : 300, (337) gives . Jo-oooooooii 241 — 0-000001738^) ( + 0-000000335^ Mass of Earth = 0-000003056537 > (0000000007043 + 0000003 423 de) I +0-000016965^ Mass of Moon — 0-012315 7 — 0-22 10 d£+ (0-000042 11 +o-ioi 5rt£) Mean distance from Earth to Sun — 92 793 504-54 857000^ ± (70993 +170 796 000 dt) miles Mean distance from Earth to Moon — 238 g 5 7 - 5 3 900 de ± (3-3 1 2 + 7 99 1 d£) miles- 112 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 26.— MASS OF THE MOON FEOM OBSERVATIONS OF THE TIDES. The first determination of the Moon's mass was made by Newton in 1687, from the tides, and other investigators have since employed the same method, but for more than 1 80 years it yielded no trustworthy result. Its failure was due to various causes, both theoretical and practical, and although some of these were cleared up by La Place as early as 18 18, there was little prospect of success until the recent application of harmonic analysis to the reduction of continuous observations of the tides, recorded by automatic gauges, and extending over long periods of time. An effort has been made to collect in the following list all the more important determinations of the Moon's mass which are based upon the method in question, but owing to the singular sparseness of bibliographic references in writings on that subject, it is difficult to esti- mate what degree of completeness has been attained. Reciprocals of the Moon's Mass, determined from Observations of the Tides. 1687. Newton, from the tides before the mouth of the river Avon, three miles below Bristol, England. (9, lib. 3, prop. 37, cor. 4.) 398 1738. D,. Bernoulli. (5, p. 549.) 70- 1818. La Place, from the tides at Brest, France, observed during the years 1807 to 1814, inclusive. (348, p. 55.) . . 69-3 1824. La Place, from a rediscussion of the above observations at Brest. (7, T. 5, liv. 13, chap. 3, \ 10.) 74-9 1831. Lubbock, from the tides at London, England, observed during the years 1808 to 1826, inclusive. (350, i83i,p. 392) 667 1854. Haughton, from the semi-diurnal tides on the coast of Ireland, observed during the year 1851. (344, p. 130.) . 63- From the diurnal tides, during the same period. (344, p. 130.) 95- i860. Lubbock remarks in his paper on the lunar theory (Mem. Roy. Ast. Soc. 1861, vol. 30, p. 29) that the observations of the tides which he employed gave him a value "probably about 1:67-3 " f°r tne ratio of the mass of the Moon to the sum of the masses of the Earth and Moon. His value of the reciprocal of the Moon's mass must therefore have been 66-3, which agrees with what he found from the tides at London, in 1831, so closely as to render it probable that they are the tides referred to. 1862. Haughton, from the semi-diurnal tides at Port Leopold, North Somerset, observed November, 1848, to July, 1849, inclusive. (345,1866^.655.) s 65-4 From the diurnal tides during the same period. (345, 1863^.253.) 85- 1866. Haughton, from the semi-diurnal tides at Frederiksdal, Greenland, observed August, 1863, to August, 1864, inclusive. (345, 1866, p. 642.) 64-6 1866. Haughton, from the semi-diurnal tides, observed at the following points on the coast of Ireland, during the year 1851. (346, p. 346.) : Bunown 69-1 Cahirciveen 64-2 Castletownsend 49-2 Dunmore East 55-0 Courtown 107-2 Kingstown ... 46-3 Donaghadee 35-1 Cushendall 21-1 Portrush 846 Rathmullan 717 Mean 60-4 1867. Finlayson, from the mean range of the spring and neap tides at Dover, England, observed during the years 1861, 1864, 1865, and 1866. (343, p. 272.) 87-9 1870. FERREL, from observations of the tides at Boston, Mass., from July I, 1847, t0 July '. 1866. (334, p. 85.) . . . 78-6 1871. FERREL, from a rediscussion of the tides at Boston, Mass., July I, 1847, to July 1, 1866, with special reference to the Moon's mass. (335, p. 198.) 75-1 1874. Ferrki., from observations of the tides at Brest, France, during the years 1812 to 1832, inclusive. (336, p. 189.) . 78-0 1874. Ferrel, from a second revision of his discussion of the tides observed at Boston, Mass., July I, 1847, to July ', 1866. (336, p. 196.) 817 ON nil SOLAR PARALLAX VND ITS RELATED CONSTAJJ ji? 1S74. Ferrel, from seven years' observations of the tides at Liverpool, England, 1857 to 1 860, and is 1'- -"') T.S74. Ferrel, from observations of the tides at Portland breakwater, England, during the years 1851, 1S57, 1866, and and 1S70. (336, p. 223.) 801 1S74. Ferrel, from observations of the tides at Fort I'oint, Cal., during the three years 1S5.S to 1S01. (336, p. 22^ 70 '. 1574. Ferkki., from observations of the tides at Karachi. India, during the three years 1S6S to 1S71. (336, p. 234.) . 7 S 1 . 1575. Ferrel, from observations of the tides made at Pulpit Cove, Penobscot Hay, Maine, during the six years 1870 to i875- (33s> P- 294) 833 1S82. Ferrel, from observations of the tides made at Port Townsend, Wash., during the three years 1874 to 1876. (339.P-44S.1 772 1882. Ferrel, from observations of the tides made at Astoria, Oregon, during the three years 1874 to 1876. {syj, p. 443.) 681 j Ferrel, from observations of the tides made at San Diego, Cal., during the three years 1869 to 1871. (339, p. 448) 880 1SS3. Ferrel, from observations of the tides made at Sandy Hook, N. J., during the six years 1876 to 1881, inclusive. (340, p. 251.) 771 Long ago Airy showed why the Moon's mass can not be accurately determined from the mere ratio of the solar and lunar effects in the semi-mensual inequality of the tides,* but nevertheless many of the values recorded above have been obtained in that very way, and are therefore worthless. Those found by La Place's method, f or by Ferrel's modification of it, are theoretically correct, at least for deep-water tides, but instead of confining ourselves to them, we shall compute many new values from the "Results of the harmonic analysis of tidal observations'' which have been published by Major Baird and Professor Darwin.}: La Place's method of deducing the Moon's mass is not adapted for use with har- monic tidal constants. We shall therefore employ Ferrel's formulae, and as much of the available data was collected by Sir William Thomson, Mr. Edward Roberts, Major A. W. Baird, R. E. and Professor G. H. Darwin, the various notations adopted by these gentlemen are exhibited in Table XIV. Ferrel used the letters A or a for the semi-range, and e or e for the epoch of a tide, and distinguished the various classes of components by the subscript suffixes i, 2,3, etc.; but for similar components occurring in the diurnal and semi-diurnal tides he used the same symbols. Thomson used the letters R and e, respectively, for the semi-range and epoch of any component, distin- guishing the various classes of components by the initials S, M, O, K, etc., and indi- cating their period by the subscript suffixes 1, 2, 3, etc.; 1 indicating a diurnal component, 2 a semi-diurnal component, 3 a terdiurnal component, and so on. Darwin used the same initials as Thomson to designate the various classes of tidal components, but his H and u are not identical with Ferrel's A and e, and Thomson's R and e. The semi-ranges and epochs of most of the tidal components are to a certain extent functions of the longitude of the Moon's node, and are therefore subject to small inequalities having a period of 18.6 years. The A's and f's of Ferrel and the R's and e's of Thomson are affected by these inequalities, but the H's and jcs of Darwin are very nearly free from them.§ In other words, the A's and e's of Ferrel and the R's and e's of Thomson belong strictly to the years during which they were observed, but the H's and h's of Darwin are reduced to what they would have been if the Moon *323, p. 360*, art. 455. f The basis of this method is very clearly explained by Airy, 323, pp. 360*, 379*, and 386* articles 455, 536, and 555. t327- § Compare 353, 18S3, p. 86, and 338, p. 282. 6987 8 n4 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. had remained always in the celestial equator, and they therefore correspond to the means of a series of observations extending over the entire period of 18.6 years, except in so far as they may be vitiated by accidental errors. In explanation of Table XIV it is only necessary to add that quantities on the same line have similar signifi- cations. For example, Ferrel's diurnal A, and «?, correspond to Thomson's Hy and ex of K,, and to Darwin's H and u of Kj; and similarly for the quantities on the other lines. Table XIV. — Notation for Harmonic Analysis of the Tides. Ferrel. Thomson and Roberts. Darwin and Baird. Name of Tide. Speed of Tide per Mean Solar Hour. H„ Ao Mian level of sea. 0 • [A A, f| K, , R| «, K, , H K Luni -solar diurnal .... 15-0410686 c g A, O . R. d O , H K Lunar diurnal 13943 035 6 5 B A3 ea P , R, El P , H K Solar diurnal 14958 931 4 0 S "3 s, . K4 t4 S4 , H K 4th of principal solar series . 60-000 000 0 0 B, 5 £ «4 <'l 2SM . K.. ea 2SM . H * 31-0158958 <>, M« . Rg e6 M„ , H K 6th of principal lunar scries . 86-9523126 Our object is to determine the mass of the Moon, and as that quantity affects only the ranges of the tidal components, and is without influence on their epochs, we shall have to deal exclusively with the H's, and not at all with the k's. Our notation may therefore be abridged by using the initials of the various tides to denote their semi-ranges, and instead of H of S, H of M, H of O, etc., we shall write simply S, M, O, etc. For the diurnal tidal oscillations of the great oceans, Professor Ferrel's expres- sions are* Ki = A1 = (o-53o6— 13-1 <*//)( 1 -f 0-230 E^Ao O = A, = 0-381 3(1 — 0-230 Ei) A0 P = A3 = (0-1730— 13-6 a»(i +0-196 Ex) A0 A4zz 0-084 0 +0-231 Ei) A0 A5 — 0-070 (1—0-231 E,) A0 (365) •336, P. 89. ON THE SOLAR PARALLAX AND ITS Kill. AMU CONSTANTS. 115 where A0, Ex, and Sju are constants to be determined from the values of A^ A . A . etc, by the simultaneous solution of three or more of the equations. As the numerical values of A4 and A5 are not contained in Baird and Darwin's list of harmonic tidal constants, we shall neglect the last two equations of (365) ; but their loss is of little consequence on account of their small weight By putting' m — 13-6 Kt— 12-98 o — 131 P 2a =. 0-462 4 Kx + 5-529 O 6 = 0613 1 Kx 4- 0-585 1 0 — 0-693 o P the remaining equations of (365) give 0 lb b'S \ = (366) 0-381 3 (1- 0-230 EO VJ ; 8? = 0040 50 - 0-3813(1-0-230 EOK? 131 (i +0-230 E^O Mass of Moon zz 0012 50 + 8/x Although this solution is in the form best adapted to give exact numerical results, it is too cuinberous for general use, and we take advantage of the smallness of Sju to add another which is briefer and not appreciably less accurate : 6u — °'l22 3° Ki+o'oi3580— °4Q5 04 P 9614 36 K, + 1*513 63 O— 10'oooooP Ex Ki — * > ' "391 56 - 3436 $M) _ P-0 (Q'453 7i — 35*7*m) 0230 Ki + 0 (0-3 20 06 — 7-90 Sju) o-23oP + 0 (0088 93 — 6-99 dpi) ^3 7) A.= ° ■_ 0-381 3(1 — 0-230 EO Mass of Moon zco 1 2 50+^yw For the semi-diurnal tidal oscillations of the great oceans, Professor Ferrel gives the expressions* S2/M2 = Rl= (0-458 2 - 36-2£//)( 1 + 0-425 5 E2) p/M%— R.2=z: + 00240(1 —0-425 5 E2) K,/M2 = K3 = (o-T256-3-2^)(i+o-4599E2) (368) L/M2 = R4 - - 0-028 6(1+ 0-228 E,) N/M, = R5 = + o-i92 2(1 -o-228E2) The second and fourth of these equations may be dismissed at once on account of their small weight, but there is a difficulty in deciding how the remaining three should be treated in order to get from them the most probable values of E2 and dp. The fundamental quantities M2, S2, K,, and N are not observed independently, but are each functions of the same observed quantities, namely, a series of heights recorded by a tide gauge, and therefore according to the theory of least squares it is the sum *336. P-9i- n6 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. of the squares of the corrections to the latter which should be made a minimum, sub- ject to the conditions of (368). But even if these heights were at hand the applica- bility of this process would be doubtful, because in the present case the larger errors probably do not follow the usual law of error. However, as the only practicable course is to deal with the derived functions M2 , S2 , etc., our discussion had better be confined to them. If, on the one hand, we take the equations as they stand, and solve by the method of least squares, the results are likely to be affected by systematic errors, because all the absolute terms have been divided by the same fundamental quantity, namely, M2 , which is itself subject to error ; and if, on the other hand, we apply a symbolic correction to M2 , then we shall have as many unknown quantities as there are equations, and the errors which should be distributed among- all the funda- mental quantities will be thrown upon M2 alone. Under these circumstances it is probably best to divide the third equation by the fifth, and thus we obtain the two equations So/M2 = B = (o-458 2 — 36-2^)(i +0-425 5E0) K,/N = C = (°"653 5— i6-6o»(i +0-459 9 E2) (369) I — 0-228E, in which each of the fundamental quantities occurs once, and only once. Here, as in (365), we give two solutions. The first is that which leads to the most exact numerical results. For it we put m — — 16-051 — 166B + 36" 2 C 2u — + 1421 1 + 7-634 3 B— 7-149 5C ^ = + 3-1409 + 3511 9C and then !4 E' = ~;± Wl (f B S/x — o'oi 2 66 36-2 + 1 5-403 E2 Mass of Moon — O'oi 2 50 + 8/jl (37o) The second solution, which is briefer than the first and not appreciably less accu- rate, is as follows : § _ 0-096 38 BC + 0127 04 B — 0-126 5 7 C — 0-004 354 3-236 72 B — io-ooo 00 C — 0-454 92 E 0 — 0-65349+ 1 6-65 8/x _B — 0-4582 + 36-2^ 0-228 C +0 300 54 — j666ju 0-194 96 — 15-406/* Mass of Moon — o*oi 2 50 + <5/* (370 Professor Ferrel treats the equations (368) in a way which differs widely from that adopted above, and which is best explained by the following- extract from his paper on the tides of Penobscot Ba\ It is readily seen from an inspection of these ('([nations that they can be satisfied only very imperfectly for Pulpit Cove, within any determined values of djx and E, and that they can be * 338, P. 297. ON THE SOLAR PARALLAX AND IIS RELATED CONSTANTS. 117 much better satisfied by multiplying the first members of the equations by an unknown constant. This constant is introduced upon the hypothesis that the tidal components arc diminished by the effect of frictiou which is as a higher power than the first power of the velocity, as I have at various times explained. Upon this hypothesis large tides arc diminished by friction more than small ones in proportion to their amplitudes, and hence where there is one large component, as the mean lunar, and a number of much smaller ones, since the amplitudes of the latter are obtained by analysis from the differences between the larger and smaller resultant tides, the smaller com- ponents are diminished more than the larger ouesin proportion to their magnitudes, unless friction is as the first power of the velocity. Accordingly, Professor Feekel multiplies the Left-hand members of the first, third, and fifth equations of (368) by a constant, which he calls c* thus reducing them to the form (S2/M2) c - RjC =r (0-458 2 — 36-2d»( 1 + 0-425 5 E2) (K,,/M2)c=R3c = (o-i25 6— 3-26»(t +0-4599^,) (372; (N / M2) c — R5c = o- 1 9 2 2 ( 1 — o- 2 2 8E2) and he adds: "By the introduction of the constant c, or one equivalent to it, I have in all cases found that the observations are better represented by theory, and a better mass of the Moon is obtained, which indicates that there is an effect due to friction or some other cause which diminishes the amplitude of the tides." If we put in — + 3-2 R,— 36-2 R3 + 16*027 R5 2« = — 0742 i Rj+ 7-1495 R3— i4-I9T Rs b = + 0-335 5 Ki — 3"5i 1 9^3- 3,I36Rs the general solution of (372) is ^ 0-192 2 — 0-043 82 E9 c = 1 — F = dju = 0-012 66 — Iw, (373) Rx( 0-192 2 — 0-043 82 E2) R5(36-2+ 1 5-403 Ej Mass of Moon rz o o 1 2 50 -f Sju or more conveniently, and with no real loss of accuracy, „ _ 0-036 52 So— o- 1 26 58 K2 — o 004 35 N ~ 0-930 5 1 S2 — 1 o-ooo 00 K, — 0-454 92 N F _ o- 1 92 20 S2 — N (0-458 20 — 36-2Qf>» . , ^ 2 ~~ 0-043 82 S2 + N (0*194 96 — 1 5-4oo» _ _ F _ (o- 1 92 20-- 0-043 82 E2) M2 Mass of Moon zr o 01 2 50 + o> The last solution shows that Professor Ferrel's process results in replacing i/Ma by an indeterminate, c/M2; and thus, instead of having four fundamental quantities This c is identical with the i -F of equations (130), (345), and (354) of his Tidal Researches. (336, pp. 75- '88, and 195.) n8 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. from which to find two unknowns, he has but three fundamental quantities from which to find three unknowns. Table XV contains a series of corrections to the Moon's mass, deduced from tidal observations made in thirty-four different ports; namely, at Brest and Boston of Ferrel's list, and at all the stations named in Baird and Darwin's list of harmonic Table XV. — Corrections to the Moon's Mass, deduced from Observations of the Tides. . o u 99 4 > 45 1 08 — 1 72 4 000073 4 131 183 4- 076 — o-ooi 83 — I 29 4 078 + 084 098 i — 088 2 25 4 0001 46 4 ' '9 + 527 095 4 0-002 77 4 o-ooi 80 4 + 2 40 278 188 4 1 23 + 043 4- 070 4 000035 — 1 16 018 4- 032 4- 002 4 0-000 84 4 051 - 275 4 204 I >\ HI!', m »LAR PARALL W AND ITS RELATED O iN I \ S 119 tidal constants where the observations extended over a period of two or more yeai together with some where they were limited to a single year. The corrections given in the columns headed Sju', d>", 6ju'" have been computed, respectively, by means of formula' (367), (371), and (374), from Baird and Darwin's harmonic constants;* and ;is the two last-mentioned formula' deal with the same 'data, we have now to consider which of them should be preferred. At St. Thomas the K2 and X tides seem unknown, or at least they are not given in Baird and Darwin's list. Rangoon is situated upon the eastern arm of the Irra- waddy River, at a distance of 21 miles from the sea; and Kidderpore is a suburb of Calcutta, on the Hooghly River, 80 miles from the sea, the width of the navigable chan- nel for 10 miles below that point being only abput 250 yards. These circumstances render it probable that the values of 6> found from the tides at St. Thomas, Rangoon and Kidderpore are untrustworthy, and accordingly we shall reject them. An examin- ation of the remaining data reveals facts which may be tabulated thus : Column dfi' 6M" 6M"' Number of plus corrections .... 16 16 24 Number of minus corrections . . 13 13 5 Sum of corrections +488 +824 +3923 If we divide each of these sums by 29, and add the quotients respectively to 0"Oi2 50, the resulting values of the Moon's mass will be 1 : 78*9, 1 : 78*2 and 1 : 72'2. The latter is so much too large as to place its erroneous character beyond doubt, and we therefore conclude that formula (371) is decidedly preferable to (374). The failure of (374) probably indicates that the height of the tides is influenced not so much by the direct effect of friction upon their amplitudes as by its indirect effect arising from the changes which it produces in the epochs of certain shallow-water components, which cannot be separated from the deep-water components with which they are combined;! and that hypothesis is further supported by the known fact that when the effects of friction and of the Earth's rotation can be regarded as of the second order, their effect upon the epochs of the oscillations is also of the second order, but upon the amplitudes it is of the third order only. J The great difference between the sums of the corrections in the columns Sju' and Sju" is probably due to the circum- stance that the diurnal tides are affected by fewer shallow-water components than the semi-diurnal ones. The wide range in the values of S/u' and Sju" shows the imperfection of our present tidal theory, and Professor Ferrel thinks its improvement depends mainly upon the study of the shallow-water terms. He adds : § With regard to the determination of the Moon's mass, from the results so far as obtained the relations of the diurnal tides promise better success in the future than those of the semi- diurnal tides. The diurnal tides are not affected by so many shallow-water components, and it is probable that these can be determined from the analysis of the observations, since there are two comparatively quite large components with periods differing from those of any others, and hence can be determined by analysis of the observations; and then from the theoretical relations t336, p- 55- 1336, P- 5'- 2338.P-299- I 20 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. given in Schedule III the others can be, at least approximately, determined, and the components of deep-water tides which they affect can be corrected for their effect. The relations of these cor- rected results, obtained from the analysis of the observations, should then agree with the theo- retical relatives, and give a correct mass of the Moon. Instead of attempting- such intricate and uncertain computations, we shall employ another method which is simpler and not less promising. It is evident from Table XV that the value of the Moon's mass given by the tides varies irregularly, not only from point to point along the coast, but also within rivers and large harbors, and even with respect to the diurnal as distinguished from the semi-diurnal tidal components ; Sju' and 6fx" having the same sign at 15 places and opposite signs at 16 places. It is therefore highly probable that the cause of these variations may justly be regarded as an accidental one, whose effect will vanish from the mean of a series of observa- tions made at a sufficient number of stations ; and if so, the best mode of treating the corrections in Table XV will be to take the mean of those given in the fourth and fifth columns. By that method the result for each station will be h(d/*' + $m"), as given in the last column of the table ; and then the question of weights arises. At first sight observations extending over a long period seem likely to be more exact than those limited to a single year, but in reality there is little difference between them, because the accidental errors at any station are generally small compared with those due to constant causes. The arithmetical mean will therefore be the most probable result, and after rejecting St. Thomas, Rangoon and Kidderpore, we have from the re- maining 29 stations in the fourth and fifth columns Sju' = -f-o-ooo 168 ±0000305 ( ~ \ V = + 0-000284 ±0-000348 ^3/5' Regarded as a single series, the 58 corrections in the fourth and fifth columns give £(£// -f- Sjli") — + 0000 226 i cooo 230 (376) while the 31 corrections in the last column give i(t the table, after which {$77) became J(tf/< -(- S/u") — — 0000018 ±0000 146 (379) Very likely (379) is nearer the truth than {377), but as no satisfactory reason can be assigned for rejecting any of the corrections, we shall adopt for Sju the value (377) with the probable error {37S) We therefore have as our final result from the tides <5 M = + 0000 2i4± 0000 222 Mass of Moon z= 00 12 7 1 4 ± 0*000 222 = (38o) 78 653 ±1374 The mass of the Moon employed in previous sections was derived from the lunar parallax, and if the probable error of the observed value of that quantity is taken to be ±0202 74", as given in Table VI, the resulting probable error of the mass is ±0000 180; whence it follows that the mass from the tides has only one-third less weight than that from the parallax. 27.— A MORE COMPREHENSIVE LEAST SQUARE ADJUSTMENT. The discussion in Sections 25 and 26 shows that the flattening of the Earth, and the mass of the Moon from the tides, should be included in the least square adjustment, and we have now to develop the equations necessary for that purpose. For the adjustment of the flattening a symbolic correction to its observed value must be introduced in the conditional equations, and we shall do that by the indirect method employed on page 1 1 1, because any other process would entail needless compli- cations. The requisite numerical data corresponding to the two values of e used on page 1 1 1 are given in Table XVI ; those for e' = 1/293-5 having been collected from pages Table XVI. — (Quantities employed in forming the Conditional Equations (382). < <•* a '3S-3 oV% Log. coefficient of 1st equation . . 2 ^T? ±-L-^ ., M ( 1 — (216 236-65 — 228 40ode) sin3 P ) o or v6 = jW — 2? < j 77J 7 5 c. j n — — TTt I ( 3-757 444 9 — o-022 9i«£ — (807 952-64 — 853 360a*) sin-* r > , Ar [4-66507071+0-4589^—10] o or v~, = 1 + M — L~ J ' —'- . .. ,7 sin1 P Proceeding as in Section 2 1 , we have next to differentiate these equations with respect to all the quantities expressed symbolically, and in doing so it must be remem- bered that (204) and (70) require that when E becomes E + dE, §£ shall become |> — 31 ji6"dE, and when e becomes £ + de, P shall become P+5062"^. The re- sults are ON rill SOLAR PARALLAX AND ITS RELATED CONSTANTS. I2t o - r, + dp + 3 ( , ^j_ M j dM - -4g d E - 0-352 5p . .fte o = V6 + rfi-|(^-3i 716" dE) + [2-9133]* 1 '//sa r ,i«, 8in2PcOsP.rfP + 3 arc 1 (# — |o"S72 46 1 il ) r — ?— -. r , . , ,, 10 v* l 0/ t j &j [5-23996— 10] — [0-572 46J sin3 P o = v7+ cCSl + 3 arc 1" cot P ( 1 + M) dP + ( 3 arc 1" cot P 5 062" — 1-056 8)(i + M) de To secure the utmost accuracy in the subsequent computations, the coefficients in (383) should be reduced to numbers with values of the quantities involved midway between the observed and adjusted ones. The following- were used, and they fulfill the required condition quite approximately : 1 p — 8809" %\= 9224" a — 20460" V = 186342 P —342267 Q= 12520 (9=497 58 M — 0012520 g = 50"358 L= 6518 £=0-000003030750 Their substitution in (383), and the addition of the appropriate v to each equa- tion, gave rise to the following expressions : ozz vx + dp + [0-4624]^^! — [5-9863] c/E — [04921]^ o = v2-\-dp — [i2459](/M — [74106— 10] dP— [88473 — io]r/Q — [11 149]^ 0 = vz-\-dp + [2'84i9]c/M — [74106— io]dP — [o i3o8]^L — [11 149] de o — i\ + dp +[56746— io](Ar+ [8-2481 — io]dO — [0-699 1 ] _rt 12 .0 oT — TS •§■ s ^ 'fa 60 CJO 0 s v. 00 «o s V J2 « rt 2 U Cn S) P3 v» 1 rfS W •» h ^ 0 a £ '3 0 0 000000 1 1 1 1 ; > 1 O Tf 0 vO 00 00 *N 00 tJ-00 CO On r^jro>-" O *-On*-OOOOOOOnO « OO N OnOnioOnOnQOl'I'OOn b r^> *- c\vb c>C\inN »■ ^*t 1 s s "o ,2 "o1 1 1 1 r- ft 00 1 8 i 0+0 T * 1 00 r~. N r-~ c» On t~~ m no r^ ». co 1 — 1 1 — 1 1 — 1 1 + + 1 — 1 O 1 NO t^ Tf V* ^ 1 * B 1 <— > •» O I (—1 1 — 1 0 ■* t-~ m U) (•) m n «« r~ m O M «* n+ J. 1 1 l__J 1 1 3> 1 1 + 1 S m «- 00 p) m Q p - yi 9 in in O O + 11 + ■8 0 On •* Q m Ov 0 CO m 0 n Oi O ~ rn + + 1 5*8 0 1 0 00 O N O VO O N 6 b\ + + •Nj ■ 0 . 0 0 . 0 6 ; + OOO '. ! 1 1 On vO 0 VO 00 w «« vo vO ri N vo c\ o^ bi ; I + 1 O O T 7 0) M "*■ CO M ■*• «*■ ON 1 1 * 0 0 8 6 + . c 0 T I 00 r» N 1^ p) On r^ m no t*. « co r-» « C\ • 1 + + 0 T ■* *» m m P) «- rn O 1 + II II II II II II II II II II II II <,p-8*)£3)o'^ B _> > W S u 00 V o >« "» g in in ro NO m 00 N 1 NO CO O 1 + + in 1-^ 0 ON co ON N ^-v "I O N N ON 0 0 O CO N« 0 0 VO •^ l 1 1 + ro NO O LTl m m ON O en vn N ^ ■* O r^ O 00 m Tt- rn Ph m M N 0 ■« ■* ** + I + 1 m CO •en i-^ N w in co 00 in m 0 NO ^ NO 0 8 vO 00 1 NO + 1 0 1 <* + 00 ■* On CN| in On in - — * 8 in NO — NO 0 ■-■ 0 + + + I 0 r~ 0 co M t*i On t^. in ON S 1 + •* + ti ri S B <7N t- vn CO •* 0 ■O rf rn •Vt M B M N m « M M m 1^ n iO O M O t- 1 + 1 1 m M On fO On CO in t~ "* _i r. r^ NO N O M O O O O + + + On m N On in On t^ NN t^» no P) t^ 00 & * m O O 8 O * O 0 0 1 0 + O l 0 1 II II ll II II 0 0 O 0 O I IN THE SOLAR PARALLAX AND I Is RELA I I ■ h CONS! \'- '25 CO 8 06 ao J£ NO X •* r» m M P) -r r-^ NO M On in *■ vO t t- 00 o "1 ON in ON ON in ■4- M M in M in M r^ M rn N On *t M en r^ O b O b + 1 1 + + 1 1 1 1 + 1 1 7 o n- m N •♦ 3 o in P< oo X o CN ■* m OO in in oo N oo tn in X> on N M On m M in NO n ■* 1- ti >* w "1 rn in 00 t^ m p NO « M o PI v£> tn pi ON On C) in On M Q PO m o O oo M in in f~ NO O Q o ■* O r^ NO NO O * « o o 6 1 b 1 b + b 1 b 1 b + b + + + 1 b + b 1 1 O oc oo *■ NO ■«*■ m ** ON r^ NO ON r^ on M oo _, r^ 00 O \r> X in m «= in r»5 on M QO • in M op r^» in O P) ro M ro u"i O oo r^ t^» 0 O 8 f) NO 8 -+ ** NO NO m t** o NO Tf w M M r^ t^ in 0 o o i O o 1 O + 1 o 1 O 1 + 1 NO 1 b + b 1 04 1 O o t^ rn M 00 M in o ■+ o oo in tJ- o On \r> X ON t^ oo o oo On oo ON On M io o rn T o -o 00 00 00 rn OO oo O oo * O ft in oo o 00 r^ O oo 00 vr» NO o o rn M o ON vO M NO rn ro r^ o o •f PO o o CI m 0 in i^ ■>*- o 8 0 O o o vO o TT o 6 1 b ! b 1 b b 1 b 1 b + 1 1 1 b b 1 O U"» 7 o NO in oo ON vO ro o io X t^ M 8 _. 00 oo On NO o 00 r^ pi 00 *5 m tort PI M Tf r^ M r-* m in PI & w PO O t^ ■* •* — t^* m N ON M M on N Tf *• ON •* r^ 6 00 O o m t^ c PI p"! rn N oo e*) T o o o in o PI O N o in o o b b b b b b b b b b 1 + + 1 + + + + + 1 1 + 9* 7 o t-» oo NO PI in o o u-j * NO r^ ■* o M r^ NO ST S ^^ \i ■y *s "e "« "§ * >» •« ->2 Ss 1.26 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. As a preliminary step toward finding the probable errors of the adjusted quan- tities, we substitute in (387) the values of vu v2l v3, etc., from (384), and thus obtain the equations (388), which are to be read in the same way as those on page 67. Then, by the process described on page 71, and with the probable errors of the observed quantities from (392), the results given in Table XVII were deduced. Reverting now to the flattening of the Earth, there can be little doubt as to what the results are from the geodetic arcs, precession and nutation, and perturbations of the Moon; and for the pendulum experiments Helmert's reduction seems best, partly because it is based upon more data than any other, and partly in consequence of the discussion on page no. Accordingly, the following observed values of f, from pages 5, 97, 95, and 102, are the only ones to be considered: Method of determination. Geodetic arcs, Clarke . . Pendulum experiments, Helmert Precession and nutation . . . Perturbations of the Moon 1 1293-47 = 0-003 407 503 I : 299-26 = 0-003 341 576 I : 297-67 = 0-003359425 I : 294-93=0-003390635 Equations No (388). 0 Logarithmic coefficients for compating- - {dp) (,/P) (4) {dm {dQ) (,/L) (#) + 9892 8 - i° — 8-469 4 — 10 — 6-667 4 — IO -S-7'3 9 - '0 — 0498 5 -87195- 10 (,/P) — 6-168 1 - 10 + 9662 5 - 10 — 5540 3— 10 + 7586 3 -10 -81348- 10 + 8-1365- 10 (rff) -77470- 10 — 8-9180 - 10 + 70634— 10 — 9-1100— 10 — 9-096 9 — 10 + 9-055 0 - 10 (<®) + 8-484 2 - 10 + 9655 2 - • 10 — 7800 6 — 10 + 9-847 2—10 + 9-834 1 - 10 — 9792 3 - 10 (*Q) — 7-2790 — • 10 — 7-212 4 — 10 — 4-7978 — 10 +' 6-844 3 — 1° + 9-987 8 - 10 + 5-987 3 - 10 (dL) — 81800- 10 + 9-893 7 - 10 + 7435 8—10 — 9-4824 — 10 + 8-667 6 - 10 + 9-5100- ■ 10 (da) + 9-435 2 -- - 10 + 9299 8 - - 10 + 6-745 2 — 10 — 8791 8 — 10 + o-593 8 + 8-839 6 - 10 (dd) + 6-886 7 - - 10 + 67513- 10 + 41967—10 — 62433— IO + 8-045 2 - 10 + 6-291 0 — 10 (,/V) + 5-504 7 - 10 + 5-369 3 - - 10 + 28147 — 10 — 4-861 3 — 10 + 6-663 3 - 10 + 4-909 1 - 10 (dE) — 4-809 6 — 4-447 i — 20713 + 4-1180 — 5967 4 — 4298 8 (,/M) + 95oi 1 - 10 + 0898 2 + 84529— 10 — 0-499 6 + 0-8584 — 0-825 x (de) — 05678 + 3-2506 — 9-406 8 — 10 + 1-453 1 — 1-6844 + 1-6113 Factors. Logarithmic coefficient.-, for computing- (da) (dd) (dV) (dE) (dU) (A) {dp) + 9'649 3 - • 10 + 10352 + 27469 — 33522— 10 + 6-3258- 10 -5734 2- 10 (,/P) + 7-2172- - 10 + 8603 1 - 10 + 0-3165 — 0-693 3—io + 5436 7- - 10 + 6-1209 - - 10 (<'?) + 80389- - 10 + 9-424 8 - - 10 + 1-1382 — 1-6935 — 10 + 6-357 3 - - 10 - 5-653 7 - 10 m — 8-776 2 — - 10 — 0-162 1 -1-875 5 + 2-430 8 — 10 — 7-094 5 - 10 + 6-390 9 - 10 W) + 7-588 3- - 10 + 8-974 2 - - 10 + 0-687 6 — 1-2904 — 10 + 4-464 0 - - 10 — 3631 1 - 10 (dL) + 8-5141- - 10 + 9-9000 — - 10 + I-6I3 3 — 2-301 7 — 10 — 7-1098 — - 10 + 6238 6 - 10 (*) + 9-5I95- - 10 — 1-211 5 + 2-5248 + 3-4476— 10 — 6-409 0 — - 10 + 5365 9- 10 (dd) — 7-2770- • 10 + 9'979 5 - - 10 + 9976 5 — 10 + 0-899 l — IO — 3860 4 - 10 + 2817 1 — 10 (dV) + 5-495 0 - - 10 + 6-88o 9 - - 10 — 8-594 3— 10 + 9-517 1 — 20 — 2-478 5 - - 10 + 1-435 4- - 10 (dE) + 5-1192 + 6-505 i + 8-223 9 + 99702 — 10 + I-73I4 — 0928 6 (dU) — 9798 1 - - 10 — 1-1840 — 2-900 8 + 3-45o 1 — 10 + 9994 2 - - 10 + 72689- 10 (de) + 0-4125 + 17984 + 35125 -43034—10 + 8-9156- 10 + 97" 1- 10 ON THE SOLAR PARALLAX AND ITS RELATED CONSTAN1 127 TABLE XVIL — Computation of the Constants rrquiri N THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. « The substitution of (389) in (381) gives (h = — 0-000032 761 (390) whence, by (70) and (75) P = 3 423-08" + 5 062" dem 3 422-914 16" ±0-121' (39 1) The values of the observed quantities employed in the more comprenensive least square adjustment are those given in (143), (391), (89), (90), (66), (67), (91), (92), (101), (132), (380), and (389), all of which are collected in (392) for convenience of reference. p = 8-834" ±00086" P ==3422-914 164" + 5 062" cte ±0121" g= 503586" — 31 71 6"rfE± 0-00248" $= 9-233 i"±o-oii 2" Q= 12546" ±035" L = 6514" ± 0-016" a — 20-466" ±0011" K^ ' 0 = 497'Os ± ro2s Vz 186347 ± 36 miles E = 0-000003 005 097 ±0-000000015056 M = 0-012714 ±0000222 e =0003 374 785 ±0000032 964 The adjustment was effected as follows: 1. To allow for the change in the flattening from 1 : 2935 in (382) to 1 : 296 3 in (392), the corrected conditional equations (393) were computed from (382) by sub- stituting therein the numerical value of de from (390). 2. The residuals, (394), were found by substituting the observed values, (392), in the corrected conditional equations, (393). 3. The corrections by adjustment, (395), were found by substituting the resid- uals (394) in the formulae (387). 4. The correctness of all the numerical processes involved in passing from (382) to (395) was checked by the well-known relation \jmn] + 100 \_an\(d£) + \bri\{dp) -f cio [cn](c/P) + [dri](d^) -f [en)(da) — [pvv] = o where [paw] is the sum of the weighted squares of the absolute terms in (385) ; [aw], [few], [en], [dti], [ew] are the absolute terms in (386); and \_pvv\ is the sum of the weighted squares of the corrections by adjustment in (395). The result of the check is given in (396). 5. The incompletely adjusted quantities, (397), were found by adding the cor- rections (395) to the observed quantities (392). ON THE SOLAR PARALLAX AND ITS RELATED l ONSTANTS. I -'<, Corrected Conditional Equations. oorv1=j)- [2784988 2j(t^m) oorv2=jp —[5*303 1248— io]PQ J — -^ ootvz—P — [4-681 9624— 10] PL - M oor„,=1,-I»2!^35] (393) [7^26028 i] o or y6 = ^ - yg ~ M "J 1 — 216 24413 sin3 P ) oor«6 = #-g J 3757445 7-807980-60 sin8 P ) [466505568-10] o or «, = 1 + M - 1 __ First set of Residuals. Vl = + 0-075 184" r5 - + 0-030 149" v2 = — 0018 582 v6 = + 0079 261 (^ 03 = + 0*294 925 r7 = + 0-000662 v4zr + 0-007 374 Firs* Approximation to the Corrections by Adjustment. (dp) --0-02487956" {da) -- 001161952' (rfP) =-0-15306762 (d0) = + roo38i4538 (dg _ + o-ooo 103 67 (dV) =-10163 88 miles (395) (<*§) = - 0-01153896 (dE)= + 0-000000050940 (dQ) =-0-510094 79 (dM) = - 0-000374748 CrfL) = + o-oo7 861 33 («k) =- 000004424841 [pm] +004555243 100 [an] (de) — 5 99Q91 [&n](a» — 2575443 o*io[cn](dP)- 553281 [*•](*» - I21 , M [en] (da) - 524440 U9°; Sum +000302867 [^w] +0003028 10 Check 000000057 G9S7- I ?0 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. First Approximation to the Adjusted Quantities. p — 8809 120" a = 20-454380" P = 3422;537 113 Q— 498-004* i>= 50357088 Vz 18633684 miles §^= 9221561 E =z 0000003056037 Q= 124-94991 M= 0-01233925 L= 6521861 e — 0003330537 (397) 6. By substituting the value of £ from (397) in (381), the corresponding value of de was found to be — o 000077 009, and by substituting that in (382) the corrected conditional equations (398) were obtained. 7. When the quantities (397) were substituted in the conditional equations (398), they gave rise to a second set of residuals (399), thus showing the adjustment to be incomplete. (396) proves that no error exists in any of the numerical operations, and it is easily seen that these residuals arise from the neglect of terms of the second order in forming the differential equations (383). 8. The better adjusted quantities (400) were obtained by substituting the residuals (399) in the formulas (387), and adding the corrections so found to the quantities (397). 9. By substituting the value of £ from (400) in (381), the corresponding value of de was found to be — 0-000076 492, and by substituting that in (382), the corrected conditional equations (401) were obtained. 10. A third set of residuals, (402), was found by substituting the quantities (400) in the conditional equations (401). Second set of Corrected Conditional Equations. oorr1 = # — [2784981 45]/ — — V ooyv2— p — [5303 1248— 10] PQ ! ±— 1 — M 1 AT oor r3= p — [4-681 962 4 — 10] PL— - - [8-91246262] , ON OOXV^—p — L ^—~ J . (393) [7526 OI 7 20l o or Vr. = )> — l / j / j oor*6=tJ-^-_J , Af [4'66s 035 xi — iol o or v1 z=. 1 + M — — — - J J J * sin^P — 2 16 254-24 sin3 P 4467 — 808 01 8-36 sin3 P ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. I 3 I Second set of Residuals. Vi =z -+■ O'ooo 1 40" vs = + o 000 008" r,- + ooooio7 ',; = + o 000 1 1 8 V3 — + 0"004 322 V7 zr + O'OOO 000 06 v4 — + 0000 030 Second Approximation to the Adjusted Quantities. p — 8 S09 050" « zz 20-454 5I3 Pr=3422"542 144 0 = 498-005 98 I8 jg = 50*357 096 v= 186 337-004 miles |lzr 9220520 E = 0000003 056095 Qzr 124-951244 M = 0-012335 279 Lzr 6522956 £ ZT 0-003331054 Third set of Corrected Conditional Equations. o or i\-p - [2-784 981 53] ( yXm) i+M o or v, —p — [5*303 1 24 8 — 1 o] PQ oorw3r=^— [4681 962 4— 10] PL i-M i+M M [7 526017 33] o or v5 — p — L/ J Tr ' -30-1 X a «- M\ 1 — 216 254-1 2 sm3P > oory6 — il — g ^ ryg' (3757446 7 — 808 017-92 snrP) , ,f [4665035 61 — 10] o or V-, — 1 + M — ^ J fJ__. sin P (399) (400) [8-912462 75] o or v^ — p — L y TT- ^" , ,. J V<9 (401) 2%ird set of Residuals. vx — -\- 0000 00 i" vb— o-ooo 000" r, = + o-ooo 00 1 v6 = — 0000 o 1 9 (4Q2) v9 — — o-ooo 040 V-, — — o-ooo 000 034 ?>4 zz OOOO OOO Z%ird A jiprori, nation to the Adjusted Quantities. }> — 8-809051" a. =20-454 5 I2" P = 3422-542 157 0 = 498-005 947s g= 50357096 Vz= 186337-002 miles (4Q3) ilzz 9-220537 E= OOOOOO3056097 Q- 124951261 Mz= OO12335305 L— 6522940 £ = 0003331057 132 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 11. The finally adjusted quantities, (403), were obtained by substituting the residuals (402) in the formulae (387), and adding the corrections so found to the quantities (400). 12. From (403) and (381) the value of de was found to be — 0-000076 489, and the resulting conditional equations from (382) were sensibly the same as (401). 13. The substitution of the quantities (403) in the conditional equations (401) gave the final residuals (404), which show that the adjustment is sufficiently complete. Final Besiduals. vx ■=. O'ooo 000" v5 rr + o-ooo 000" v2 == + 0*000 000 v6 — + o-ooo 006 , . v3 — -\- o-ooo 00 1 v7 = + o-ooo 000 003 Vt rr — O'OOO OOO The data and results of the computation outlined in (393) to (404) are given iu Table XVIII, but it yet remains to explain how the probable errors attached to the various quantities were derived. Putting r" for the probable error assumed for a quantity of weight unity in equation (188), m for the number of observation equa- tions in (385), n for the number of unknowns they contain, and \_pvv\ for the sum of the weighted squares of the corrections by adjustment, we have in accordance with the procedure described on pages 70 and 7 1 *=^(S) (405) With r" = O'Oi, m z= 1 2, n — 5, and the values of p and v from (385) and the third column of Table XVIII, (405) gives q= 1-4091. The probable errors in Table XVIII result from the multiplication of that value of q into the respective probable errors in (392) and the respective values of Ra in Table XVII. The following explanations relate to the quantities appended to Table XVIII : The masses of Mercury, Venus, and the Earth, together with their probable errors, were computed by means of formulae (344), (345), and (346), with the value of dFi rb dFi' given in the fourth column of Table XVIII. The mass of the Moon is that given in the table, transformed from a decimal to a vulgar fraction. The lengths of the equatorial and polar semi-diameters of the Earth were found from (356), with the value of e from the fourth column of Table XVIII, and de from (381). As the expressions (356) are of the form a = m -f- n.de, if we put r with a sub- script letter for the probable error of the quantity symbolized by the subscript, we shall have ra2 = rm2 + (n>\)2 (406) ON THE SOLAR PARALLAX AND I l> RELATED CONSTAN'I 133 Table XVIII.— Final Results for the Epoch L850.0. Quantities. Observed values. 1 lorrections by ail- justment. Adjusted values. // // // // // P 8-834 4: 0-012 12 0024 95 8809 05 -)- 0005 67 V 3422-69281-!- 0-17050 — o- 1 50 65 3422542 16 J- 012533 i1 50-356994. 000349 + o-ooo I I 50357 10 J- 0003 49 % 9-2331 -t 00157s — 0-012 56 9-220 54 -J- o-ooS 59 '2 1 2546 4- 0493 iS — 0-508 74 124-951 26 4. 0081 97 L 6-514 -j^ 0-02255 + o-ooS 94 652294 J- 0-01854 a 20466 J- 0015 50 — o-oi 1 49 2045451 -|- 0-01258 e 4970s J- 1-437 2S« + 1-005 95s 498005 95° 4. 0-30834* V 186347 -J- 50728 miles — 9-998 miles 186337-00 -J- 49-722 miles E o-ooo 003 005 097 _|- o-ooo 000 022 625 }+ 51000 | 0-000003 056097 . -J- o-ooo 000 005 829 M 0012 714 J- 0000 312 820 }- 378 695 { 0012335305 -{-0-000036 214 e 0003 374 785 -j- 0000 046 450 }- 43 728 { 0003331057 -j- 0000 032 37 1 Mass of Mercury = g!358 223 ±0-072441 = ^_1_ 3000000 83746724=1765762 Mass of Venus = °'^2 ^7 ±°'°°* 5°3 = . Mass of Earth = Mass of Moon = 401847 4089684^1874 _ 1-084 720 ± 0002 069 __ 1 354 936 3272144=624 81-0684=0-238 Earth's equatorial semi diameter = Earth's polar semidiameter One Earth quadrant a 20 925 293 ±4094 feet, — 3 963-1244= 0-078 miles. = 20S55 5904=325-1 feet, = 3 94992 2 4-0062 miles. = 393 775 8r9±4 927 inches, = 32 814 652 ±4106 feet, — 6 2 14-896 ±0-078 miles. 1 Earth's flattening- — a 300-205 4= 2964 Mean distance from Earth to Sun = 92 796 950 4= 59 715 miles. Mean distance from Earth to Moon = 238 85475 4= 9 916 miles. Length of seconds pendulum = 3251045+0017356 sin2 cp feet, = 39'Oi 2 540 + 0-208 268 sin2 cp inches. Acceleration by gravity, per second of mean time = 32-086 528 + 0-171 293 sin2 cp feet, — 97798864-0052 2 10 sin2 9) meters. '34 ON THE SOLAR RARALLAX AND ITS RELATED CONSTANTS. Table XVIII gives r£ = db 0*000032 371, and upon the assumption that the probable error of the length of a well measured geodetic arc is about one part in 150000, (356) gives rmfora = ± 139-5 feet rm for b z= ± 1390 feet With these values the probable errors attached to the adjusted lengths of the Earth's seniidiameters were found from (406). A quadrant of the Earth, measured from the north pole along any meridian to the equator, is the theoretical basis of the metric system, and in computing its length from our values of the Earth's polar and equatorial seniidiameters the following formula was employed : One Earth Quadrant ^(q+.&))+27o(r7+-J+etC- (407) The distances of the Sun and Moon from the Earth, together with their probable errors, were computed by means of the formula D — a cosec^ rb s/[(cosecj> . ra)2 + (D cot^ arc 1" rp)2] (408) where a is the Earth's equatorial semidiameter, ra its probable error, D the distance corresponding to the parallax p, and >-pthe probable error ofjj. The expression for the probable error of D was found in the usual way, by differentiating a cosec^J, squaring the several terms, and replacing the differentials by the probable errors. The equations (321) and (12) give '=<<--? 45 - esnr q> . TOrt . , (409) from which the length of the seconds pendulum was computed with the adjusted values of a and e from Table XVIII, ?45from (10) and ^from (17). The expression for the acceleration by gravity then followed from the usual formula, g — ttH. Replacing sin2

COS 2ffl ( 2— £ ) t* I 2 — 8) + {la — T2(T \2C0S 2

COS (2G0' + 29°04') — o-ooo 135 5 p~5f sin3

P- 339- ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. 137 -+- 0*000 738 6 p ~ c f sin3 cp — ^ sin cp \ cos cos (r«/ -}- 30 02') + o-ooo 217 5 p~°f sin2

(418) and by equating (417) and (418) (™* _ e\ sin2 cp - P sin2 cp' + P (sin3 cp' -^ sin cp'^j (4 1 9) At the poles cp — cp', and as all powers of the sine are there unity, (419) reduces to ezzi^-P^P (420) hh 5 or, with our adjusted values of a, /0 and tx £ = 0-00866952 — P=Fo-4P' (421) in which the double sign is to be taken negative for the northern, and positive for the southern hemisphere of the Earth. To distinguish the two values of e thus arising, we shall call the former e\ and the latter e". In 1818, from pendulum experiments at 31 stations, Bessel foundf P — + 0-005 444 8 P' — + o-ooo 668 9 whence, by (421) £' = 1:338-17 e" — 1 1286-34 %(e' + e")= 1:310-11 In 1 84 1, from experiments at 54 stations, Dr. C. A. F. Peters foundj P = + 0-005 233 F = — 0-000334 * 1, p. 130. f 1, p. 131. Ji09,p. 170. I38 ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. whence e' — 1 : 280-10 e" zz 1 : 30276 J(e' -f *") r= I : 290*99 In 1872, from experiments' at 74 stations, Nyrkn found* P = + 0*005 ] 94 1J' = _ o*ooo 1 34 whence f'zz 1:283*36 £"zz 1 1292-23 £(N rtiE SOLAR l'AKAl.l AX AND ITS RELATED CONSTAX 139 Log. p = 9-999 2772 758 + 0-0007245325 COS 2CP — 00000018 131 cos 4

— q> =688-2242" sin 2 Mean density of the Earth = 5-576 +; 0016 Surface density of the Earth =z 2*56 ±016 Moments of inertia of the earth, (C — A) : C = 0-003 2^5 21 = 1: 306-259 C — A = o'ooi 064 767 EVr A = 13 = 0-325 029 K a 0 = 0-326 094 E'rr Length of the Seconds Pendulum. I — 390 1 2 540 + 0-208 268 sin2 finches, = 3251 045 +0-017 356 sin2

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[Die nurnerische Bestiromung der Triigbeitsmomeute der Erde. ] Ast. Nach., 1842, Bd. 19, S. 197-198. 288. Haughton (Rev. Samuel). On the density of the earth, deduced from the experiments of the As- tronomer Royal, in Harton coal-pit. L., E. aud D. Phil. Mag., 1856. vol. 12, pp. 50-51. 289. Hill (G. W . i. On the interior constitution of the earth as respects density. Annals of Mathematics, edited by Prof. Oruiond Stone, University of Virgiuia, 1888, vol. 4, pp. 19-29. 290. Hutton (Chas.). An account of the calculations made from the survey and measures taken at Schehallien, iu order to ascertain the mean density of the earth. Phil. Trans., 1778, pp. 689-788 291. Hutton (Chas.). The mean density of the earth. Being an accouut of the calculations made from the survey aud measures taken at Mouut Shichal- lin, in order to ascertain the mean density of the earth. Improved from the Philosophical Trans- actions, vol. 68, for the year 1778. i6o ON IIII'. soi.AR PARALLAX AND ITS RELATED ((INSTANTS. 291. Hutton (Chas.) — Continued. Tracts on mathematical and philosophical sub- jects. » * - By Chas. Hutton, ix. i>. and F. R. s., etc. Vol. 2, tract 26, pp. 1-63. London, 1812, 12nio. 384 pp. 292. Hutton (Charles). On the mean density of the earth. Phil. Trans., 1821, pp. 276-292. 29:5. Jolly (Ph. von). Die Auwendnng der Waage auf Probleme der Gravitation. Zweite Abhandlang. Abhandlangen der Mathematisch - l'hvsikali- scbeu Classe der Kouiglich Bayerisehen Akadeuiie der Wissenschaften, 1883, Bil. 14, 2te Abtheilun^. pp. 1-26. 294. Le Gendre (A. M.). Suite des recherches sur la figure des planetes. Histoire de l'Acadeiuie des Sciences (Paris), 1789. pp. 372-454. 295. Levy (Maurice). Sur la th6orie de la figure de la terra. Comptes Rendus, 1888, t. 106, pp. 1270-1276, 1314-1319, and 1375-1381. 296. Lipschitz (R. }. Versuch zur Herleitung eiues Gesetzes, das die Dichtigkeit fiir die Schichten ini Inueru der Erde anuiihernd darstellt, ausden gege- benen Beobachtuugeu. Journal fiir die reiue und angewaudte Mathe- matik (Borchardt. Berlin), 1863, Bd. 62, pp. 1-35. 297. Lipschitz (R.). Beitrag zur Theorie des Gleich- gewichts eiues nicht honiogenen lltlssigen rotireu- den Spharoids. Journal fiir die reiue und angewaudte Mathe- inatik (Borchardt, Berlin), 1863, Bd. 63, pp. 2>9-295. 298. Maskelyne (Rev. Nevil) An account of observa- tions made on the mountain Schehallien for find- ing its attraction. Phil. Trans., 1775, pp. 500-542. 299. Mendenhall (T. C). Determination of the ac- celeration due to the force of gravity, at Tokio, Japan. Amer. Jour, of Science, 1880, vol. 20, pp. 124-132. 300. Mendenhall (T. C). On .t determination of the force of gravity at the summit of Fujiyama, Japan. Amer. Jour, of Sience, 1^81, vol. 21, pp. 99-103. 301. Plana (Jean). Note sur la deusite" moyenne de l'ecorce superticielle de l-i terre. Ast. Nach., 1852, Bd. 35, S. 177-191. 302. Playfair (John). Account of a lithological survey of Schehallien, made in order to determine the specific gravity of the rocks which compose that mountain. Phil. Trans., 1811, pp. 347-377. 303. Poincare (H.). Sur la figure de la terre. (On the relation between interior density, flattening, Clai- raut's equation, and precession.) Comptes Rendus, 1888, t. 107, pp. 67-71. 304. Poincare (H). Sur la figure de la terre. Bulletiu Astrouomique, (Paris) 1889, t. 6, pp. 5-11, and 49-60. 305. Poynting (J. H.). On a method of using the bal- ance with great delicacy, and on its employment to determine the mean density of the earth. (1 plate.) Proc. Roy. Soc, 1878-9, vol. 28, pp. 2-35. 306. Radau(R.). Sur la loi des densit6s a l'iut<5rieur de la terre. Comptes Rendus, 1885, t. 100, pp. 972-974. 307. Radau (R.). Remarques sur la th6orie de la figure de la terre. Bulletiu Astronomique, 1835, t. 2, pp. 157-161. 308. R[adau] (R.). Revue des— Sterneck (R.)— Unter- snchungen iiber die Schwere im Innern der Erde. Bulletiu Astronomique (Paris), 1887, t. 4, pp. 234-237. 309. Reich (P.). Versuche iiber die mittlero Dichtig- keit der Erde. inittclst der Drehwa^c von F.Reich, Prof, der Physik an der K. S. Bergakademie. Mit 2 lithographirten Tafeln. Freiberjr, 1838. 12mo, 66 pp. [I have never seen this work, but on ac- count of its historical importance I quote the title from 271, p. 9.— W. H.] 310. Reich (P.). Neue Versuche mit der Drehwage zur Bestimmung der mittleren Dichtigkeit der Erde. Abbaudluugen der matbematisch-physischeu Classe der Koniglich Sachsischen Gesellschaft der Wissenschaften zu Leipzig, 1853, Bd. l,pp. 383-430. 311. Roche (Edouard). Mdmoire sur l'e'tat interieur du globe terrestre. Par M. fidouard Roche * * * Paris, 1881. 4to, 43 pp. (Extrait des Mdmoires de l'Acad6mie des Sciences et Lettres de Montpel- lier. Section des Sciences, tome 10.) 312. Roche (Edouard) Note sur la loi de ladensit6 a l'iuterieur de la tern-. Comptes Rendus. 1854, t. 39, pp. 1215-1217. 3124. Schell (Anton). Leber die Bestimmung der mitt- leren Dichtigkeit der Erde, vou Anton Schell, Professor am Baltischen Polytechuicum zu Riga. Mit drei lithographirten Tafeln. Goettingen, 1809. 4to, 39 pp. 313. Sterneck (Robert von). Uutersuchungen fiber die Schwere ini Innern der Erde. Mittheilungen des kaiserl. konigl. Militiir-Geo- graphischen Institutes (Wien), 1882, Bd. 2, pp. 77-120. 314. Sterneck (Robert von). Wiederholung der Un- tersuchungen fiber die Schwere im Innern der Erde. Mittheilungen des kaiserl. konigl. Militar-Geo- graphischen Institutes (Wien), 1883, Bd. 3, pp. 59-94. 315. Sterneck (Robert von). Untersuckungen fiber die Schwere auf der Erde. Mittheilungen des kaiserl. konigl. Militiir-Geo- graphischeu Institutes (Wien), 1884, Bd. 4, pp. 89- 155. 316. Stieltjes. Note sur la density de la terre. Bulletin Astronomique (Paris), 1884, t. 1, pp. 465-467. 317. Tisserand (P.). Quelques remarques au sujet de la theorie de la figure des plauetes. Comptes Reudus, 1884, t. 99, pp. 399-403 and 518. 318- Tisserand (P.). Sur la theorie de la figure de la terre. Comptes Rendus, 1884, t. 99, pp. 577-583. 319. Tisserand (P ). Quelques remarques au sujet de la theorie de la figure des planetes. Bulletin Astronomique (Paris), lb84, t. 1, pp. 417-420. ON THE SOLAR PARALLAX AND ITS RELATED CONSTANTS. [6l 320. Tisserand (F.). Sur la constitution interioure do la terre. Bulletin Astronomiquo (Paris), 1884, t. 1, pp. 521-527. 321. Todhunter (I.). A history of the mathematical theories of attraction, and the figure of the earth, from the time of Newton to that of Laplace. By I. Todhunter ■ * * London, 1873. 2vols.,8vo. Vol. 1, pp. xxxvj+476 ; vol. 2, pp. 508. 322. Wilsing (J.). Bestimmung der mittleren Dichtig- keit der Erde mit Hiilfe cines Pendelapparates. Publicationen des Astrophysikalischcn Obser- vatoriunis zu Potsdam, Bd. 6, S. 31-128 (1887, Nr. 22); 2te Abhaudlung, Bd. 6, S. 129-192 (1889, Nr. 23). THE TIDES. 323. Airy (Sir Geo. B.). Tides and waves. Encyclopaedia Metropolitana. 2nd Division, Mixed Sciences, vol. 3 pp. 241*-396*. (London, 1842. 4to.) 324. Airy (Sir Geo. B.). On the laws of the tides on the coasts of Ireland, as iuferred from an exten- sive series of observations made in connection with the Ordnance Survey of Ireland. Phil. Trans., 1845, pp. 1-124. 325. Airy (Sir Geo. B.). On a controverted point in Laplace's theory of the tides. L., E. & D. Phil. Mag., 1875, vol. 50, pp. 277-279. 32G. Airy (Sir Geo. B.). On the tides at Malta. Phil. Trans., 1878, pp. 123-138. 327. Band (Maj. A. W.) and Darwin (G. H.). Results of the harmonic analysis of tidal observations. Proc. Roy. Soc, 1885, vol. 39, pp. 135-207. 328. Baird (Maj. A. W.). A manual for tidal observa- tions, and their reduction by the method of har- monic analysis; with an appendix containing auxiliary tables to facilitate the computations. By Major A. W. Baird, R. E., F. R. S., * * * London, 1886. 8vo, pp. vi+54-f xl. 329. Challis (Jas.). On the mathematical principles of Laplace's theory of the tides. L. , E. & D. Phil. Mag., 1875, vol. 50, pp. 544-548. 330. Darwin (G. H.). Tides. Encyclopaedia Britaunica (ninth edition, Edin- burgh, 1888), vol. 23, pp. 353-381. 330J. Darwin (G. H.). Second series of results of the harmonic analysis of tidal observations. Proc. Roy. Soc, 1889, vol.45, pp. 556-611. 330J. Darwin (G. H). On the harmonic analysis of tidal observations of high and low water. Proc. Roy. Soc, 1890, vol. 48, pp. 278-340. 331. Darwin and Turner. On the correction to the equilibrium theory of tides. I. By Prof. G. H. Darwin. II. By Mr. H. H. Turner. Proc. Roy. Soc, 1886, vol. 40, pp. 303-315. 332. Evans (Captain F. J. O.) and Thomson (SirWm.). On the tides of tbe southern hemisphere and of the Mediterranean. Report of the 48th meeting of tho British Asso- ciation for the Advancement of Science, 1878, pp. 477-481. 33:?. Ferrel (Win.). The problem of the tides, with re- gard to oscillations of the second kind. The Astronomical Journal (Cambridge, Mass.), 1856, vol. 4, pp. 173-176. G987 11 340. 341. 334. Ferrel (Wm.). Discussion of tides iii Boston harbor. Report of the Superintendent of the D. 8. Coast Survey, 186ft Appendix 5, pp. 51 L02. 335. Ferrel (Wm.). On the moon's mass as deduced from ;i discussion of the I ides of lioston harbor. Report of the Superintendent of the r. s. Coast Survey, 1*70. Appendix 20, pp. 190 199. 336. Ferrel (Wm.). Tidal researches. An appendix to the II. S. Coast Survey Report for 1-7 1, but printed separately. 4io, pp. xiii-j 268. :*37. Ferrel (Wm.). On a controverted point in La place's theory of the tides. L., E. &, D. Phil. Mag., 1876, vol. 1, pp. 182 187. 338. Ferrel (Wm.). Discussion of tides in Penobscot Bay, Maine. Report of the Superintendent of the U. S. Coast and Geodetic Survey, 1878. Appendix 11, pp. 268-304. 339. Ferrel (Wm.). Discussion of the tides of the Pa- cific coast of the United States. Report of the Superintendent of the U. S. Coast and Geodetic Survey, 1882. Appendix 17, pp. 437-450. Ferrel ( Wm.). Report on the harmonic analysis of the tides at Sandy Hook. Report of the Superintendent of the U. S. Coast and Geodetic Survey, 1883. Appendix 9, pp. 247- 251. Ferrel (Wm.). Description of a maxima and mini- ma tide-predicting machine. (5 plates.) Report of the Superintendent of the U. S. Coast and Geodetic Survey, 1883. Appendix No. 10, pp. 253-27 2. Ferrel (Wm.). Laplace's solution of the tidal equations. The Astronomical Journal ( Boston, Mass.), 1880, vol. 9, pp. 41-44 ; and 1890, vol. 10, pp. 121-123. Finlayson (H. P.). On the mass of the moon as deduced from tho mean range of spring and neap tides at Dover during the years 1861, 1864, lsu5, and 1866. Month. Not., 1867, vol. 27, p. 271. 344. Haughton (Rev. Samuel). Discussion of tidal observations made by direction of the Royal Irish Academy in 1850-51. Transactions of the Royal Irish Academy, 1854, vol. 23, Part II, pp. 35-140. Haughton (Rev. Dr. Samuel). On the tides of the Arctic seas. Parts 1 to vn. Phil. Trans., 1863, pp. 243-272; 1866, pp. 639- " 655; 1875, pp. 317-360; and 1878, pp. 1-16. Haughton (Rev. Dr. Samuel). On the semi- diurnal tides of tho coasts of Ireland, deduced from tho Academy observations. Parts 1 to xi. Transactions of the Royal Irish Academy (Dub- lin), 1871, vol. 24, Science, pp. 195-211, and 253- 350. 347. Houzeau (J. C.) and Lancaster (A.). [Bibliog- raphy of tides.] (Thcone des marees. La uiarfo et la rotation du globe.) Bibliographic g. 298-312. Thomson (J. J.) and Searle (G. F. C). A determi- nation of" r, " the ratio of the electromagnetic unit of electricity to the electrostatic unit. Proc. Roy! Soc, 1890, vol. 47, pp. 376-378 \ I NDEX. Page. Aberration, constant of 25 adjusted value of the constant of .73, 108, 111, 133, 142 no satisfactory theory of 144 Adjusted quantities, constants necessary for find- ing 127 sources of their probable errors 142 Airy, Sir Geo. B 4,7,8,9,12,13,14,15,17,18,34,52, 53, 89, 90, 91, 97, 113, 101, 143 Alembert, J. lo R. d' 58 Algebraic notation 1 Angle of the vertical, formula for 139 Anomalistic month, length of 16 Asten, E. von 34,35 Asteroids, solar parallax from observations of. . . 51 Authorities, mode of citing 1, 146 Auwers, A 24,25,26 Ayrton, W. E 135 Backlund, O 34 Bailie, J. B 89,90 Bailly, J. S 28 Baily,F 89,90,97 Baird, Maj. A. W 113,114,115,118,119 Ball, L. de 25 Bernoulli, D, 112 Bessel, F. W 4, 13, 23, 24, 25, 34, 35, 36, 86, 87, 93, 137 Bibliography 146 Biot, J. B 6,8 Bolto 24 Bond, G. P 35,36 Bond, W. C 51,54 Borda, J. C 6,7 Boreneus, H. G 97 Bouguer, P 3,89,90 Bouvard, A 34,35 Bradley, Jas 23,24,25,26,44,51,101 Breen, H 21 Brinkley, John 25,26 Biirg, J. T 101 Burckhardt, J. C 20,34,101 Buscb, A. L 25,26 Campbell, James 19 Carlini, F 89,90,91 Cassini, J. D 51 Cavendish, H 89,90 Page. Centrifugal forco at the surface of the Earth .. . 56 Citation of authorities, modo of 1, 146 Clairaut, A. C 9,94,97 Clarke, Gen. A. E 3,4,5,9,89,90,91,90,97,98, 102,109,110,111,126,138 Clarke, F. W 91,92 Coast Survey, arcs projected by the United States 143 Computations, how made 146 Comstock, Gen. C. B 143 Concluding remarks 142 Conditional equations, general forms of 56 Constants, desiderata for improvement of astro- nomical 145 Copeland, Ralph 35 Cornu, A 29,30,33,89,90 Corrections by adjustment, numerical values of. 68, 108 Cruls, L 52,53 D'Alembert, J. le R 58 Damoiseau, M. C. T. de 13,20 Darwin, Geo. H 98,113,114.115,118,119 Day, length of sidereal 10, 139 Delambre, J. B.J 3,28,34,52 Delaunay, Ch 17,18,60,62 Density of the Earth 89,139 Desiderata for improvement of astronomical con- stants 145 Distances of the Sun and Moon. See under Sun and Moon. Distances of Sun and Moon, formula for probable error of 72,134 Diurnal tidal oscillations, Ferrel's expressions for 114 Downing, A. M. W 25,26,27,51,54 Dreyer, J. L. E 24 Du Sejour, D 52 Earth, centrifugal force at surface of 56 density, flattening, and moments of inertia of B9 observed mean density of 89, 139 observed surface density of 91, 139 Le Gendre's law of density of interior of 95 adjusted value of eccentricity of 138 adjusted value of flattening of 110, 111, 133, 138 flattening of, found from perturbations of the Moon 165 i66 IX HEX. \ Tage. Earth, etc. — Continued. flattening of, Hansen's formula for finding, from perturbations of the Moon 100 flattening of, Pontdcoulant's formula for finding, from perturbations of the Moon. 100 values of the flattening of, found by various authors, from perturbations of the Moon. 101 flattening of, deduced from precession and nutation 92 flattening of, found by various authorities from pendulum experiments 97,137,138 uncertainty respecting the flattening of 142 uncertainty in the flattening of, and its effect upon the other constants 102 mass of.. 34,42,49 adjusted mass of 73,108,111,133,140 general expression for adjusted mass of 107 moments of inertia of 93,99,100,101,102, 139 table of processional moment of inertia of, according to various authors 93 lunar inequality of motion of 19 formula for lunar inequality of motion of. .. 62 adjusted value of lunar inequality of mo- tion of 73,108,111,133,140 eccentricity of orbit of 11, 140 perturbations of plane of orbit of 74 morion of perigee of , 45 perturbations of, by Mars 45 perturbations of, by Venus 45 formula for rail ins of 139 size and figure of 3,109,133,136, 138 quadrant, formula for length of... 134 quadrant, length of 133, 138 Eastmau, J. R 51,54 Eccentricity, of the Earth..." 138 of the Earth's orbit 11,140 of the Moon's orbit 18,140 Ecliptic, obliquity of 22, 79, 80, 80, 141 perturbations of plane of 74 Electric constant, v 135 Encke, J. F 33,34,37,52,53 Euler, Leonhard 52 Enlerian nutation, period of 145 Exner, Franz 135,136 Ferrel, Wm 112, 113, 114, 115, 110, 117, 118, 119 Ferrer, J. J.de 52 Finlayson, H. P 112 Fischer,A 97,136 Fizcau.H.L 29,33 Flamstead, John 51 Flattening of the Earth, found from pendulum experiments, according to various authori- ties 97,137,138 found from perturbations of the Moon 98 found from precession and mutation 92 uncertainty respecting 142 Forbes, G 30,33 Foucault, L 29,33 Frisby, Edgar 146 Galle, J.G 51,54,55 Geodetic formula) 3,5,104,109,134 Page. Gill, David 51,54,55 Gilliss, Jas. M 51,54 Giulio, Chas.1 89,90 Glasenapp, S 28 Gould, B.A 51,54 Gravity, acceleration by 133, 139 Gyld6n, J.A.H 26,27 Haerdtl, E. von 34, 35 Hall, Asaph 2G, 27, 34, 35, 36, 51, 54, 146 Sail, Asaph, jr 35,36 Hall, Maxwell 51,54 Hansen, P. A. ..10, 11, 12, 13, 15, 10, 17, 18, 19, 34, 37, 38, 61, 62, 78, 80, 86, 87, 93, 98, 100, 101, 102, 142 Harkness, Wm 53,91 Harmonic analysis of the tides, notation used by various authors in the 114 Haughton, S 89,112 Helmert, F. R 8, 9, 97, 102, 110. 126, 142, 143 Henderson, Thos 20, 21 , 26, 51, 54 Herschel, Sir F. W 35 Hill, Geo. W 34,37,3^,39,41,97,98,100,102,130 Himstedt, F 135 Hind, J. R 35 Hockin, C 135 Holden, E. S 35,36 Bornsby, Thomas 52 Horrox, Jeremiah 44 llnttou, Charles 89,90 Inclination of the Moon's orbit 18,140 Indian arc, effect of, on computed length of the Earth's polar semidiameter 143 Introduction 1 James, Sir Henry 89,90,91 Jolly, Ph. von 89, '.10 Jupiter, mass of 34,35,42, 140 Kilometer, length of 3 King, W. F 135,136 KlemenSic, Ignaz 135 Kohlrausch, R. H. A 135, 136 Krueger, A. 34,35 Kiistner, F 26,27 Lacaille, N. L. de 20,51 La Condamine, C. M. de 3,89,90 LaGrange, J. L 33,34,35 Lake Survey, arcs measured by the United States 143 Lalande, J. J. le F. de 24,52 Lamont, J 35 La Place. P. S. de 6,8,34,35,86,87,93,94,98, 99, 101, 112. 113 Lassell, W 35,36 Latitude, period of variation of 145 Least square adjustment, general formula for the 64,106,122 a more comprehensive 121 LeGendre, A. M 92,94,95,96,98,102,143 LeGeudrc's law of density of the interior of tho Earth 95 INDEX. 167 Tago. Length, relations between standards of 3 Le Verrier, U. J ... 10, 1 1, 12, 19, 22, 34, 35, 36, 40, 41, 42, 44, 45, 73, 74, 75, 76, 78, 79, 80, 86, 87, 93, 94 L6vy, M 98 Lexell, A.J 52 Light equation, the 28 adjusted value of 73, 108, 111, 133, 14-2 Light, observed velocity of 29 adjusted value of velocity of 73, 108. 111,133, 142 Lindenau, B. von 26,27,31 Lindhagen, D. G 26,27 Lindsay, Lord 51,54 Lipschitz, K 98 Lubbock, Sir J. W 112 Lunar inequality of Earth's motion 19 inequality of the Earth's motion, adjusted value of 73,108,111,133,140 parallax 20 parallax, adjusted value of 73,108,111, 133, 140 Luni-solar precession. Sec under Precession. Lundahl, G 25,26,27 Maclear, Sir Thomas 26.27 Main, Robert 25,26,27 Mars, mass of 31,35, 42, 140 motions of its perihelion, eccentricity, incli- nation and node 43 position of, in 1672 44 solar parallax from observations of 51 Marth, A 35,36 Maskelyne, Nevil 28,52,89,90,101 Mass of Moon, formula for. 60,105,122 (See Moon.) Masses of the planets 33,42,49, 140 (See under name of each planet.) formula' for changes in, on account of cor- rections by adjustment 68, 107 formulae for probable error of 49,107 Mathieu, C. L 6,8 Maxwell, James Clerk 135, 136 M'Kichan, Dugald 135,136 Mean density of the Earth 89,139 M.xbain, P. F. A 3 Mendenhall, T. C 89,90 Mercury, longitude of node of 36 mass of 33,42,49 general expression for adjusted mass of 107 adjusted mass of 73,108,111,133,140 motion of node of 40 Meter, length of 3 Michelson, A. A 29,30,33 Midler, A 34,35 Moments of inertia of the Earth. ..93,99, 100, 101, 102, 139 Mouth, length of 12,139 anomalistic 16 nodical - 16 sidereal 15, 139 synodical 16, 139 tropical 16 Moon, distance of 73, 108, 110, 111, 133, 140 formula for probable error of distance of. . . . 72, 134 eccentricity of orbit of 18, 140 inclination of orbit of 18, 140 adjusted mass of 73,108, 111, 133, 140 mass of, from observations of the tides.. 112, 118, 121 Moon, etc. — Continued. expressions for computing mass of, from diurnal tidal osoillationa 115, 116, 117 expressions for computing massof, from semi- diurnal tidal oscillations 115, 116, 117 n 1 can sidi nal motion of 13 motion of node of 16,140 parallactic inequality of in formula for parallactic inequality of 00 adjusted value of parallactic inequality of. . . 7;:, 108, 111,1:::!, Ill parallax of 20 adjusted value of parallax of 73,108,111,133,140 Neison, E 19 Neptune, mass of 36, 42, 140 Newcomb, Simon. .12, 13, 14,15,16, 17 I- !3,30,33, 34,35,36,51,54,61,62, 138 Newton, Sir Isaac 34, 35, 112 Nicolai, F. B. G 34 Node, motion of Moon's 16, 140 Nodical mouth, length of 16 Notation, key to algebraic 1 Notation of various authors for harmonic anal- ysis of the tides 114 Nutation, constant of 25 formulae for adjusted values of 79,141 formula for, in terms of the precession and lunar parallax 60, 105, 122 Dr. Peters's formula for 87 adjusted value of 73, 108, 111, 133, 141 period of Etilerian 145 Nyr6n, Magnus 23,24,25,26,27,137,138 Obliquity of ecliptic 22,79,80,86,141 Obrecht, A 53,54 Observed quantities, values of 68,106,128,133 Olufsen, C. F. R 10,11,20,21,34,37,38 Parallactic inequality of the Moon's motion 18 Parallactic inequality of the Moon, adjusted value of 73, 108, 111, 133, 141 Parallax. See Solar Parallax, and Lunar parallax. Paris line, length of 3 Pauckcr, M. G. von 97 Pechmann, E 89,90 Peirce, Benjamin 35, 120 Pendulum, formuhe relating to. .6, 7, 9, 56, 97, 103, 134, 137 length of the seconds 6, 133, 136 ad j usted length of tho seconds 1 39 Perry, John 135 Perturbations. See under Mercury, Venus, Earth, and Mars. Peters, C. A. F 25,26,27,86,87,93,137 Piazzi, G 23,25,26 Picard, J 41 Pingre", A. G 52 Plana, Jean 34,91,98 Planets, masses of 33, 42, 49, 140 Planman, A 52 Playfair, John 89,90,91 Poiucare", H 9? Poisson, S. D "• 8 Pout6coulant, G. de 10° 1 68 INDEX. Page. Pound, James 51 Powalky, C 34.52,53 Poynting.J. H 89,90 Pratt, John H 136 Precession, constant of 22 formula for changes in the luui-solar, on ac- count of corrections hy adjustment 69 additional formula for 73 algebraic formula for changing the funda- mental equinox and ecliptic 80,85 adjusted value of 73,108,111,133,141 and nutation, numerical formula; for 79,141 complete numerical formula for, applicable to any equinox or ecliptic 86, 141 table of values of, given by various astron- omers - 87 Probable errors, of observed quantities, corrected values of 70,132 of the adjusted quantities, constants neces- sary for finding 127 of adjusted quantities, sources of 142 of planetary masses, method of computing. 49, 107 Puiseux, V. A 52,53 Reich, F 89,90 Results, summary of 13- Richardson, W 26 Richer, J 44 Roberts, Edward 113,114 Robinson, T. R 25 Roche, E 98 Roemer, O 44 Rosa, E. B 135 Rosse, Earl of 35 Rothman.R. W 34 Rowland, II. A 135 Sabine, Gen. Sir Edwai d 6, 8, 9 Safford, T. H 35 Saigey, J. F 7 8,9,89,90 Saturn, mass of 35, 42. 140 Schjellerup, H. C. F. C 23,24 Schubert, Gen. T. F. de 4 Schur.W 34,35 Schweizer, K. G 26 Searle, G. F. C 135 Seconds pendulum, length of the 6,133,136 adjusted length of the 139 Semi-diurnal tidal oscillations, Ferrel's expres- sions for 115 Serret, J. A 22,59,77,79,92,93 Shida, R 135 Short, James 52 Sidereal day, length of 10, 139 month, length of 15 year, length of 10 Solar parallax, formula for, in terms of the Earth's mass 57, 58, 105, 122 formula for, in terms of P, L, E and M 63, 122 formula for, in terms of P, Q, E and M 61.1 22 formula for, in terms of V and a 63, 122 Page. Solar parallax, etc. — Continued. formula for, in terms of V andO 63, 122 trigonometrical determinations of 51,54 from observations of Asteroids 51 from observations of Mars 51 from photographic observations . 53 from transits of Venus 51,138 adjusted value of 73,108,111,133,140 Standards of length, relations between 3 Sterneck, R. von 89,90,91 Stockwell, John N 88 Stokes, Sir Geo. G 100 Stone, E. J 19, 21, 25, 51, 52, 53, 54, 58, 59 Struve, F. G. W 25,26,27 Struve, H 35 Struve, Ludwig 24 Struve, Otto 23,24,35,86,87 Sun and Moon, ratio of mean sidereal motions of. 17, 139 Sun, distance of 73, 108, 110, 111, 133, 140 Sun, parallax of. See Solar parallax. formula for probable error of distance of 72, 134 adjusted value of parallax of 73, 103, 111, 133, 140 equation of center 45 Summary of results 138 Supplementary data 136 Surface density of the Earth 91, 139 Sy nodical month, length of 16,139 Tait, P. G 94 Taylor, T. G 51,54 Thomson, J. J 135 Thomson, Sir Wm 94, 113, 135, 136 Tidal oscillations, Ferrel's expressions for the diurnal 114 Ferrel's expressions for the semi-diurnal 115 Tidal observations at thirty-four different sta- tions, Moon's mass computed from 118, 121 Tides, notation used by various authors in the harmonic analysis of 114 Tisserand, F 34,44,98 Todd, D. P 53,54 Toise, length of 3 Transits of Venus, solar parallax from 51,138 Transit of Venus Commission, United States 38,54 Tropical month, length of 16 Tropical year, length of 10 Tupman, G. L 52,53 Unferdinger, F 7,8,9,97,143 Units of length, relations between 3 Uranus, mass of 35,42, 140 v, the electric constant 135 Velocity of light, observed value of 29 adjusted value of 73,108,111,133,142 Venus, longitudes of 41 mass of 34,42. 19 adjusted mass of 73,108,111,133,140 general expression for adjusted mass of 107 longitude of node of 37 motion of node of 40 Vertical, formula for angle of 139 INDI-A. I 69 Page. Wagner, A 2(>/27 Weber, W. E 135, 13C Weisse, Maximilian 23 Wilsing, J 89,90 Winnecke, A 51,54 Woodward, R.&..J. 14G 6987 12 Warm, J.P 34,36 Year, length of the sidereal 1". 139 length of the tropical 10, I ■"■' Young, James 30 Zi I